US20030162067A1 - Fuel water vapor replenishment system for a fuel cell - Google Patents

Fuel water vapor replenishment system for a fuel cell Download PDF

Info

Publication number
US20030162067A1
US20030162067A1 US10/368,425 US36842503A US2003162067A1 US 20030162067 A1 US20030162067 A1 US 20030162067A1 US 36842503 A US36842503 A US 36842503A US 2003162067 A1 US2003162067 A1 US 2003162067A1
Authority
US
United States
Prior art keywords
fuel
heat
fuel cell
cell stack
heat exchanger
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US10/368,425
Inventor
James McElroy
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bloom Energy Corp
Original Assignee
Ion America Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ion America Corp filed Critical Ion America Corp
Priority to US10/368,425 priority Critical patent/US20030162067A1/en
Assigned to ION AMERICA CORPORATION reassignment ION AMERICA CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MCELROY, JAMES F.
Publication of US20030162067A1 publication Critical patent/US20030162067A1/en
Assigned to BLOOM ENERGY CORPORATION reassignment BLOOM ENERGY CORPORATION CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: ION AMERICA CORPORATION
Assigned to U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT reassignment U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BLOOM ENERGY CORPORATION
Assigned to BLOOM ENERGY CORPORATION reassignment BLOOM ENERGY CORPORATION RELEASE BY SECURED PARTY (SEE DOCUMENT FOR DETAILS). Assignors: U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT
Abandoned legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/06Combination of fuel cells with means for production of reactants or for treatment of residues
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/06Combination of fuel cells with means for production of reactants or for treatment of residues
    • H01M8/0662Treatment of gaseous reactants or gaseous residues, e.g. cleaning
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/04Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/04Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
    • H01M8/04007Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids related to heat exchange
    • H01M8/04014Heat exchange using gaseous fluids; Heat exchange by combustion of reactants
    • H01M8/04022Heating by combustion
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/24Grouping of fuel cells, e.g. stacking of fuel cells
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/10Fuel cells with solid electrolytes
    • H01M8/12Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte
    • H01M2008/1293Fuel cells with solid oxide electrolytes
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2250/00Fuel cells for particular applications; Specific features of fuel cell system
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2250/00Fuel cells for particular applications; Specific features of fuel cell system
    • H01M2250/40Combination of fuel cells with other energy production systems
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2250/00Fuel cells for particular applications; Specific features of fuel cell system
    • H01M2250/40Combination of fuel cells with other energy production systems
    • H01M2250/405Cogeneration of heat or hot water
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2300/00Electrolytes
    • H01M2300/0017Non-aqueous electrolytes
    • H01M2300/0065Solid electrolytes
    • H01M2300/0068Solid electrolytes inorganic
    • H01M2300/0071Oxides
    • H01M2300/0074Ion conductive at high temperature
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/02Details
    • H01M8/0202Collectors; Separators, e.g. bipolar separators; Interconnectors
    • H01M8/0247Collectors; Separators, e.g. bipolar separators; Interconnectors characterised by the form
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/02Details
    • H01M8/0271Sealing or supporting means around electrodes, matrices or membranes
    • H01M8/028Sealing means characterised by their material
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/04Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
    • H01M8/04007Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids related to heat exchange
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/04Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
    • H01M8/04082Arrangements for control of reactant parameters, e.g. pressure or concentration
    • H01M8/04089Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants
    • H01M8/04111Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants using a compressor turbine assembly
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/04Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
    • H01M8/04082Arrangements for control of reactant parameters, e.g. pressure or concentration
    • H01M8/04089Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants
    • H01M8/04119Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants with simultaneous supply or evacuation of electrolyte; Humidifying or dehumidifying
    • H01M8/04126Humidifying
    • H01M8/04141Humidifying by water containing exhaust gases
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00Fuel cells; Manufacture thereof
    • H01M8/04Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
    • H01M8/04291Arrangements for managing water in solid electrolyte fuel cell systems
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02BCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02B90/10Applications of fuel cells in buildings
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/30Hydrogen technology
    • Y02E60/50Fuel cells
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S429/00Chemistry: electrical current producing apparatus, product, and process
    • Y10S429/901Fuel cell including means for utilization of heat for unrelated application, e.g. heating a building

Definitions

  • Fuel cells generate electricity from hydrogen or various hydrocarbon fuels.
  • an oxygen containing gas such as air
  • hydrogen or a hydrocarbon fuel is provided onto the anode side of the electrolyte.
  • the fuel cell generates electricity through an electrochemical reaction.
  • oxygen containing air is provided onto the cathode side of a solid ceramic electrolyte
  • a hydrocarbon fuel is provided onto the anode side of the electrolyte.
  • Fuel cells operate more efficiently when the oxygen content of the inlet air is higher, primarily because the Nernst potential of the cell increases when the partial pressure of oxygen is higher. Therefore, the oxygen content of air being provided into the fuel cell is sometimes increased or enriched using various processes, including pressure swing adsorption (e.g., QuestAir Inc.'s Pulsar technology), oxygen-selective membranes (e.g., Boyer et al., J. Appl. Electrochem., p.1095, 1999), or magnetic separation devices (e.g., Nitta et al., U.S. Pat. No. 6,106,963, incorporated herein by reference in the entirety).
  • pressure swing adsorption e.g., QuestAir Inc.'s Pulsar technology
  • oxygen-selective membranes e.g., Boyer et al., J. Appl. Electrochem., p.1095, 1999
  • magnetic separation devices e.g., Nitta et al.,
  • One preferred embodiment of the present invention provides a system, comprising a solid oxide fuel cell stack, and an enthalpy wheel which transfers product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply.
  • Another preferred embodiment of the present invention provides a system comprising a solid oxide fuel cell stack, at least two adsorbent beds which transfer product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply.
  • Another preferred embodiment of the present invention provides a system comprising a solid oxide fuel cell stack, and a first means for transferring product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply.
  • Another preferred embodiment of the present invention provides a method of hydrating fuel provided into a solid oxide fuel cell stack, comprising providing a hydrocarbon fuel into an anode input of solid oxide fuel cell stack, and transferring product water vapor from a fuel cell stack anode exhaust into a fuel cell stack fuel supply.
  • FIGS. 1 - 5 are schematic representations of oxygen enrichment systems according to the first preferred embodiment.
  • FIGS. 6 - 10 D are schematic representations of a combined electrical power generation and cooling system according to the second preferred embodiment.
  • FIG. 11 is a schematic side cross sectional view of a prior art solid oxide fuel cell.
  • FIG. 12 is a schematic illustration of oxygen transport through the electrolyte.
  • FIGS. 13, 15 and 16 are schematic side cross sectional views of solid oxide fuel cells according to the third preferred embodiment.
  • FIG. 14 is a schematic side cross sectional view of a prior art multi-layer solid oxide electrolyte.
  • FIGS. 17 - 24 are schematic side cross sectional views of methods of making the electrolyte according to the third preferred embodiment.
  • FIGS. 25 - 26 are schematic side cross sectional views of fuel cells according to the fourth preferred embodiment.
  • FIGS. 27A and 27B are schematic diagrams of systems according to the fifth preferred embodiment.
  • FIGS. 28 - 35 are schematic representations of seals according to the sixth preferred embodiment.
  • FIGS. 36 - 48 are schematic representations of the repeating elements of a fuel cell stack, including the felt current conductor/flow distributor elements, according to the seventh preferred embodiment.
  • FIGS. 36 - 45 are cross-sectional, exploded views and FIGS. 46 - 48 are three dimensional cut away views.
  • the inventors have realized that the oxygen content of air being provided into the fuel cell can be increased using a temperature sensitive adsorption cycle.
  • the temperature sensitive adsorption cycle utilizes the heat generated by the fuel cell during power generation.
  • the use of heat generated by a fuel cell for increasing the oxygen content of the inlet air stream in a cyclical adsorption separation process increases the efficiency of power generation.
  • heat generated by means other than the fuel cell may be used instead.
  • an air stream (a mixture of nitrogen and oxygen) is passed through a cool adsorbent medium that selectively removes a fraction of the nitrogen, resulting in a gas stream that has a higher oxygen content than the original stream.
  • adsorbent saturated with nitrogen under the process conditions, heat generated from the fuel cell operation or from another source is transferred to the adsorbent medium, and the nitrogen is driven out of the adsorbent medium through a vent. Thus, a separation is effected.
  • FIG. 1 schematically illustrates the temperature sensitive oxygen enrichment system 1 .
  • the system includes an air source 3 , an adsorbent medium 5 and a fuel cell 7 .
  • the air source 3 may be an air blower, an air inlet conduit and/or any other device which provides air into the adsorbent medium 5 .
  • the adsorbent medium 5 may be any medium which selectively adsorbs nitrogen compared to oxygen.
  • the adsorbent medium 5 is a bed containing a nitrogen adsorbing material, such as a zeolite or a mixture of zeolites.
  • zeolite such as a zeolite or a mixture of zeolites.
  • silver X, sodium X or calcium A zeolites may be used.
  • the fuel cell 7 may be any fuel cell into which air is provided.
  • the fuel cell 7 is a solid oxide fuel cell.
  • other fuel cells such as PEM, direct methanol, molten carbonate, phosphoric acid
  • the system 1 also preferably contains a heat transfer conduit 9 located between the fuel cell 7 and the adsorbent medium 5 .
  • the conduit 9 transfers heat from the fuel cell 7 to the adsorbent medium 5 .
  • the conduit 9 may comprise any device than may transfer heat from one location to another.
  • the conduit 9 may comprise a pipe, a duct, a space between walls or even a solid heat transfer material.
  • the conduit 9 is a pipe which transfers a heat transfer fluid through the system 1 .
  • An air inlet 11 is located in the adsorbent medium 5 housing.
  • the inlet provides air from the air source 3 into the adsorbent medium 5 .
  • An oxygen enriched air conduit 13 is located between the adsorbent medium 5 and the fuel cell 7 .
  • the conduit 13 may be pipe, duct or open space which provides oxygen enriched air from the adsorbent medium 5 to the fuel cell 7 .
  • the heat transfer conduit 9 comprises a pipe which is located adjacent to the fuel cell 7 , adjacent to a heat sink 15 and adjacent to the adsorbent medium 5 .
  • the conduit 9 is wrapped around the housing of the adsorbent medium 5 and around the fuel cell 7 .
  • the conduit 9 also passes through the heat sink 15 .
  • the heat transfer conduit 9 transfers a heated heat transfer liquid, such as water, from adjacent to the fuel cell 7 to the adsorbent medium 5 .
  • the heated heat transfer liquid heats the adsorbent medium 5 to desorb nitrogen from the adsorbent medium 5 .
  • the heat transfer conduit 9 also transfers a cooled heat transfer liquid, such as water, from adjacent to the heat sink 15 to the adsorbent medium 5 .
  • the cooled heat transfer liquid cools the adsorbent medium 5 , which allows the adsorbent medium 5 to adsorb nitrogen from air that is being provided from inlet 11 .
  • the conduit 9 is filled with a heat transfer liquid.
  • This liquid may be any liquid which is capable of transferring heat.
  • this liquid is water.
  • other liquids, such as mineral oil, etc., or even heat transfer gases may be used.
  • the liquid is provided through conduit 9 and through at least one valve.
  • the conduit 9 contains an outlet valve 17 and an inlet valve 19 .
  • the outlet valve 17 is preferably a three way valve which directs the liquid either through a first segment 21 of the conduit 9 , through a second segment 23 of the conduit 9 , or prevents liquid flow through the conduit 9 .
  • first segment 21 which is located adjacent to the fuel cell 7 , then the liquid is heated by the heat generated in the fuel cell 7 .
  • located adjacent means that the first segment 21 of the conduit 9 is wrapped around the fuel cell 7 or a stack of fuel cells if more than one fuel cell is used.
  • located adjacent also includes any other configuration of segment 21 which allows the fuel cell 7 to heat the liquid in the segment 21 .
  • the segment 21 may be located in contact with one or more surfaces of the fuel cell 7 or segment 21 may be located near the fuel cell, rather than being wrapped around the fuel cell.
  • the heated heat transfer liquid is then provided from the first segment 21 through the inlet valve 19 into the portion of conduit 9 that is located adjacent to the adsorbent medium 5 .
  • “located adjacent” means that the conduit 9 is wrapped around the housing of the adsorbent medium 5 .
  • “located adjacent” also includes any other configuration of conduit 9 which allows the heat transfer liquid to heat the adsorbent medium 5 .
  • the conduit 9 may be located in contact with one or more surfaces of the adsorbent medium 5 or conduit 9 may be located near the adsorbent medium 5 , rather than being wrapped around it.
  • the heated heat transfer liquid heats the adsorbent medium 5 and desorbs the nitrogen adsorbed in the adsorbent medium 5 .
  • the valves 17 and 19 are switched to provide the heat transfer fluid through a second segment 23 of the conduit 9 .
  • the second segment 23 is located adjacent to a heat sink 15 .
  • the heat sink 15 may comprise any thing which can cool the liquid in the second segment 23 of the conduit 9 .
  • the heat sink 15 may be a cooling tower, a heat exchanger, a radiator with cool air, a cold air blower or even a portion of segment 23 which runs through the cool ground or wall.
  • the segment 23 may pass through the heat sink 15 or be placed in contact with or adjacent to the heat sink 15 , depending on what type of heat sink is used.
  • the cooled heat transfer liquid is then provided from the second segment 23 through the inlet valve 19 into the portion of conduit 9 that is located adjacent to the adsorbent medium 5 .
  • the cooled heat transfer fluid cools the adsorbent medium 5 while air from inlet 11 is passing through the adsorbent medium 5 to desorb nitrogen from the air.
  • the heat transfer liquid is provided through the conduit 9 in a closed control loop.
  • the system 1 of FIG. 2 operates in a batch or non-continuous mode.
  • the heat transfer liquid is passed through the second segment 23 adjacent to the heat sink 15 .
  • the cooled heat transfer liquid cools the adsorbent medium 5 to adsorb the nitrogen from the air.
  • the heat transfer liquid is passed through the first segment 21 adjacent to the fuel cell 7 .
  • the heated heat transfer liquid heats the adsorbent medium 5 to desorb the nitrogen.
  • the system 1 operates in a continuous mode.
  • the system 100 contains two or more adsorbent mediums 5 A, 5 B, as shown in FIG. 3.
  • elements with like numbers to elements in FIGS. 1 - 2 are presumed to be the same.
  • the other adsorbent medium 5 B is heated by the heat from the fuel cell to desorb the nitrogen from the adsorbent medium 5 B.
  • the system 100 shown in FIG. 3 contains the following elements.
  • the system 100 contains one or more air sources 3 , such as blowers, and a plurality of adsorbent mediums 5 A, 5 B which selectively adsorb nitrogen compared to oxygen. While only two mediums are shown in FIG. 3, there may be more than two mediums if desired.
  • the system 100 also contains a plurality of heat transfer conduits 9 A, 9 B which transfer heat from the fuel cell (not shown in FIG. 3 for clarity) to the plurality of adsorbent mediums 5 A, 5 B.
  • the conduits 9 A, 9 B are located between the fuel cell and the plurality of adsorbent mediums 5 A, 5 B.
  • FIG. 1 There are also a plurality of air inlets 11 A, 11 B into the plurality of adsorbent mediums 5 A, 5 B, and a plurality of outlets 13 A, 13 B (i.e., a plurality of oxygen enriched air conduits) which provide oxygen enriched air from the plurality of adsorbent mediums 5 A, 5 B to the fuel cell.
  • the conduits 13 A, 13 B are located between the plurality of adsorbent mediums 5 A, 5 B and the fuel cell.
  • the system 100 contains seven three way valves, as will be described in more detail below. However, more or less than seven valves may be used as desired.
  • the system 100 contains least one inlet selector valve 27 located between the air source 3 and the plurality of adsorbent mediums 5 A, 5 B. The inlet selector valve 27 directs air from the air source 3 into either a first adsorbent medium 5 A or into a second adsorbent medium 5 B.
  • the system 100 also contains at least one outlet selector valve 29 located between the plurality of adsorbent mediums 5 A, 5 B and the fuel cell.
  • the outlet selector valve 29 directs oxygen enriched air into the fuel cell through oxygen enriched air conduits 13 A, 13 B, 13 C from either the first adsorbent medium 5 A or from the second adsorbent medium 5 B.
  • the system 100 contains at least one venting selector valve 31 located between the air source 3 and the plurality of adsorbent mediums 5 A, 5 B.
  • the venting selector valve 31 directs desorbed nitrogen to be vented through vent 25 from either the second adsorbent medium 5 B or from the first adsorbent medium 5 A.
  • At least one connecting conduit 33 is provided such that it connects a plurality of oxygen enriched air conduits 13 A, 13 B.
  • the connecting conduit 33 directs purging air from one of the first or the second adsorbent medium to the other one of the first or the second adsorbent medium to purge the nitrogen from the receiving medium.
  • the conduit 33 contains one or more flow restrictors 35 .
  • the restrictors 35 restrict the flow of oxygen enriched air, such that the majority of the oxygen enriched air exiting an adsorbent medium is directed to the fuel cell through conduit 13 C, rather than through the connecting conduit 33 .
  • the system 100 contains at least one heat transfer fluid inlet valve 37 A, 37 B located in the heat transfer fluid conduits 9 A, 9 B. Preferably there are two such valves as shown in FIG. 3. Valve 37 A directs heated heat transfer fluid to the one of the adsorbent mediums 5 A, 5 B from the fuel cell stack, while valve 37 B directs cooled heat transfer fluid to another one of the adsorbent mediums 5 A, 5 B from the heat sink.
  • the system 100 contains at least one heat transfer fluid outlet valve 39 A, 39 B located in the heat transfer fluid conduits 9 A, 9 B.
  • Valve 39 A directs heated heat transfer fluid from the adsorbent mediums to the heat sink
  • valve 39 B directs cooled heat transfer fluid from the adsorbent mediums to the fuel cell.
  • conduits 9 A, 9 B actually comprise two segments of one common conduit 9 .
  • the output of conduit 9 A is provided through valve 39 B, the fuel cell stack and valve 37 A to input of conduit 9 B, while the output of conduit 9 B is provided through valve 39 A, the heat sink and valve 37 B to input of conduit 9 A.
  • the valves 37 A, 37 B and 39 A, 39 B may be set such that the conduits 9 A and 9 B remain separate, as will be discussed in more detail below.
  • valves are set to allow the first adsorbent medium 5 A to provide oxygen enriched air into the fuel cell, while the nitrogen is desorbed from the second adsorbent medium 5 B.
  • the first adsorbent medium 5 A is cooled by a cool heat transfer fluid in conduit 9 A, while the second adsorbent medium 5 B is heated by a hot heat transfer fluid in conduit 9 B.
  • valve positions are switched as shown in FIG. 4.
  • the valves are set to allow the second adsorbent medium 5 B to provide oxygen enriched air into the fuel cell, while the nitrogen is desorbed from the first adsorbent medium 5 A.
  • the second adsorbent medium 5 B is cooled by a cool heat transfer fluid in conduit 9 B, while the first adsorbent medium 5 A is heated by a hot heat transfer fluid in conduit 9 A.
  • the system 100 can operate in a continuous rather than in a batch mode.
  • At least one adsorbent medium may be used to provide oxygen enriched air into the fuel cell, while another adsorbent medium may be heated and purged to desorb nitrogen adsorbed therein.
  • Air from the air source 3 is directed to the inlet selector valve 27 , which directs air into at least one of plurality of adsorbent mediums.
  • the valve 27 directs the air into the first adsorbent medium 5 A but not into the second adsorbent medium 5 B.
  • the first adsorbent medium 5 A is cooled by the heat transfer fluid in the first heat transfer conduit 9 A, and first adsorbent medium 5 A selectively adsorbs nitrogen from the air.
  • the oxygen enriched air exits the first adsorbent medium 5 A and is selectively directed to the fuel cell through the oxygen enriched air conduits 13 A, 13 C and the outlet selector valve 29 .
  • the inlet selector valve 27 prevents air from flowing from the air source 3 into the second adsorbent medium 5 B. Furthermore, the outlet selector valve 29 prevents flow from the second adsorbent medium 5 B to the fuel cell. Thus, no oxygen enriched air flows from the second adsorbent medium 5 B into the fuel cell.
  • a portion of the oxygen enriched air flows from the first adsorbent medium 5 A through conduit 13 A, the connecting conduit 33 and the conduit 13 B into the second adsorbent medium 5 B.
  • the flow restrictor(s) 35 in the connecting conduit 33 ensure that only a small portion of the oxygen enriched air flows into the second adsorbent medium 5 B.
  • This oxygen enriched air from the first adsorbent medium 5 A is used as purging air for the second adsorbent medium 5 B to purge the nitrogen from the second adsorbent medium 5 B.
  • the second adsorbent medium 5 B is heated by the heated heat transfer fluid in the conduit 9 B to desorb the nitrogen in the second adsorbent medium 5 B while the purging air is passing through the second adsorbent medium 5 B.
  • the desorbed nitrogen is selectively directed to be vented from the second adsorbent medium but not from the first adsorbent medium by the venting selector valve 31 .
  • the heat transfer fluid is directed in the system 100 shown in FIG. 3 as follows.
  • the heat transfer fluid is passed through a heat sink to cool the heat transfer fluid.
  • the cooled heat transfer fluid is selectively directed to the first adsorbent medium 5 A through the “cool inlet” in the heat transfer fluid inlet valve 37 B and through conduit 9 A.
  • the cooled heat transfer fluid from the first adsorbent medium 5 A is selectively directed through conduit 9 A and through the “cool outlet” in the heat transfer fluid outlet valve 39 B to the fuel cell.
  • the heat transfer fluid from valve 39 B is passed adjacent to the fuel cell to heat the heat transfer fluid.
  • the heated heat transfer fluid is then selectively directed to the second adsorbent medium 5 B through the “hot inlet” in the heat transfer fluid inlet valve 37 A and through conduit 9 B. Then, the heated heat transfer fluid from the second adsorbent medium 5 B is selectively directed through conduit 9 B and through the “hot outlet” in the heat transfer fluid outlet valve 39 A to the heat sink.
  • the inlet selector valve 27 prevents air from flowing from the air source 3 into the first adsorbent medium 5 A. Furthermore, the outlet selector valve 29 prevents flow from the first adsorbent medium 5 A to the fuel cell. Thus, no oxygen enriched air flows from the first adsorbent medium 5 A into the fuel cell.
  • a portion of the oxygen enriched air flows from the second adsorbent medium 5 B through conduit 13 B, the connecting conduit 33 and the conduit 13 A into the first adsorbent medium 5 A.
  • the flow restrictor(s) 35 in the connecting conduit ensure that only a small portion of the oxygen enriched air flows into the first adsorbent medium 5 A.
  • This oxygen enriched air from the second adsorbent medium 5 B is used as purging air for the first adsorbent medium 5 A to purge the nitrogen from the first adsorbent medium 5 A.
  • the first adsorbent medium 5 A is heated by the heated heat transfer fluid in the conduit 9 A to desorb the nitrogen in the first adsorbent medium 5 A while the purging air is passing through the first adsorbent medium 5 A.
  • the desorbed nitrogen is selectively directed to be vented from the first adsorbent medium but not from the second adsorbent medium by the venting selector valve 31 .
  • the heat transfer fluid is directed in the system 100 shown in FIG. 4 as follows.
  • the heat transfer fluid is passed through a heat sink to cool the heat transfer fluid.
  • the cooled heat transfer fluid is selectively directed to the second adsorbent medium 5 B through the heat transfer fluid inlet valve 37 B and conduit 9 B.
  • the cooled heat transfer fluid from the second adsorbent medium 5 B is selectively directed through conduit 9 B and the heat transfer fluid outlet valve 39 B to the fuel cell.
  • the heat transfer fluid from valve 39 B is passed adjacent to the fuel cell to heat the heat transfer fluid.
  • the heated heat transfer fluid is then selectively directed to the first adsorbent medium 5 A through the heat transfer fluid inlet valve 37 A and conduit 9 A. Then, the heated heat transfer fluid from the second adsorbent medium 5 A is selectively directed through conduit 9 A and the heat transfer fluid outlet valve 39 A to the heat sink.
  • conduits 9 A and 9 B comprise segments of the same conduit because the heat transfer fluid makes a complete loop through the system 100 .
  • the valves 37 A, 37 B, 39 A and 39 B may be set such that the heated heat transfer fluid returns to the fuel cell after heating one adsorbent medium, while the cooled heat transfer fluid returns to the heat sink after cooling the other adsorbent medium.
  • adsorbent mediums i.e., beds containing adsorbent medium
  • adsorbent mediums can be connected in various different ways to achieve the desired oxygen enrichment continuously.
  • FIG. 5 illustrates another system 200 according to a third preferred aspect of the first embodiment.
  • the system 200 of FIG. 5 is similar to the system 100 of FIGS. 3 and 4, except that the adsorbent mediums 5 A, 5 B are heated by the hot air emitted by the fuel cell 7 , rather than by a heat transfer liquid.
  • the air is provided from inlet 11 A into the first adsorbent medium 5 A.
  • nitrogen is adsorbed, and oxygen enriched air is provided through conduits 13 A, 13 C and valve 29 into the cathode side input of the fuel cell 7 .
  • No air is provided into the second adsorbent medium 5 B from inlet 11 B due to the position of valve 27 in FIG. 5, similar to that of the system 100 illustrated in FIG. 3.
  • the heat transfer conduit 9 is connected to the cathode side output of the fuel cell 7 .
  • the hot air exits the cathode side output of the fuel cell 7 and enters the conduit 9 .
  • the hot air then reaches a hot air selector valve 41 which directs the hot air into a first segment 9 A or a second segment 9 B of the conduit 9 .
  • the valve 41 is set to direct the hot air into the second segment 9 B.
  • the heated air from the fuel cell 7 heats the second adsorbent medium 5 B to desorb nitrogen from the adsorbent medium. After the hot air passes through conduit 9 B, the air is either vented through vent 43 B or reused for some other purpose.
  • the second adsorbent medium 5 B is used to provide oxygen enriched air into the fuel cell 7 , then the position of the valves 27 , 31 , 29 and 41 is reversed (similar to that shown in FIG. 4), and the first adsorbent medium 5 A is heated by the hot air from the fuel cell 7 to desorb the nitrogen from the first adsorbent medium 5 A. The hot air is then vented through vent 43 A or put to some other use.
  • the fuel cell 7 also contains a fuel input 45 on the anode side and a fuel output 47 on the anode side.
  • the adsorbent mediums 5 A, 5 B may be cooled by external air or by another heat transfer conduit (not shown in FIG. 5) to adsorb the nitrogen from the air passing from inlets 11 A, 11 B through the adsorbent mediums 5 A, 5 B into conduits 13 A, 13 B.
  • the heat transfer gas i.e., hot air
  • the system 200 operates in a continuous mode.
  • conditioning of the incoming air may be valuable.
  • the inlet air may be dried, heated, or cooled depending on its initial state.
  • adsorbent material it is desirable to select the adsorbent material to optimize both gas separation and rapid heat transfer.
  • the pressure drop through the bed should be minimized in order to reduce the capital and operating costs of the blower.
  • the particle size, bed geometry, and overall system layout and design may be optimized to minimize the pressure drop.
  • the adsorbent material in different beds may be the same or different depending on the system requirements.
  • an oxygen enrichment system may consist of three adsorbent beds operating in parallel, similar to the two beds shown in FIG. 2.
  • Each bed will contain 1 kg of AgX zeolite pellets with a standard mesh size of 20 ⁇ 30.
  • the beds will have a parallelipiped geometry and will contain a network of heat transfer surfaces, preferably made of metal foam.
  • the temperature sensitive adsorption process to enrich the oxygen content of air of the first embodiment is not limited to providing oxygen enriched air to a fuel cell. This process may be used to provide oxygen enriched air for any other suitable use. For example, the efficiency of a combustion process (such as a gas turbine) may increase if the inlet air is oxygen-enriched, as inert nitrogen will not need to be heated.
  • High powered electrical appliances pose challenges for thermal management.
  • Large electrical power consumers such as co-located computers or fabrication machinery dissipate most of the electrical energy provided as heat. In order to maintain appropriate operating conditions this heat needs to be removed.
  • electrical power is required to drive the appliances and to operate a cooling mechanism.
  • Certain distributed power systems offer new perspectives. Power generators such as solid oxide fuel cells provide electrical power and high quality waste heat. This heat can be utilized to drive a cooling device, thereby reducing the electrical power requirement.
  • the inventors have realized that appropriate choice of the equipment involved can provide a system where electrical power requirements and cooling requirements can be ideally matched.
  • a power generator which includes a fuel cell, such as a solid oxide fuel cell, a heat pump, and an electrical power consuming appliance, such as a computer, form an ideally matched system with respect to electrical power requirements and cooling requirements.
  • Solid oxide fuel cells typically generate approximately the same amount of heat as electrical power. This heat is available at elevated temperatures, usually in the range of 250° C. to 1000° C., and is suitable to drive a heat driven heat pump.
  • the electrical power supplied by the fuel cell is consumed by an appliance. Part of the electrical power supplied to an appliance is dissipated as heat. A close look at this part of the system reveals that all of the electrical power supplied to the appliance, which is not stored in the appliance or transmitted from the appliance beyond the system boundaries is dissipated. For most appliances, such as computers or machinery, only a small fraction of the power supplied is transmitted beyond system boundaries and most of the electrical energy supplied is dissipated as heat. The dissipated heat needs to be removed in order to avoid excessive temperatures within the appliance.
  • the inventors have realized that the system described above has the extremely convenient feature of matching cooling loads with electrical loads.
  • the combination of the heat driven heat pump with the solid oxide fuel cell provides electrical supply and cooling capacity matching the requirements of many electrical appliances.
  • Such a system is convenient, because it requires neither additional cooling devices, nor additional electrical power of significance (i.e., over 10% of the total power) to be incorporated.
  • Careful selection of the power generator and the heat driven heat pump can provide matched cooling and heating for a variety of applications.
  • the power generator can also be a combination of a solid oxide fuel cell and a gas turbine, such as a bottoming cycle gas turbine.
  • the amount of cooling and electrical power provided can be adjusted by selecting the appropriate operating conditions for the fuel cell. If for example the fuel cell is supplied with an excess of fuel, more high temperature heat can be created and thereby more cooling power. This adjustment can be especially important in situations where additional heat loads need to be removed.
  • One example for an additional heat load is heating of the conditioned appliance due to high ambient air temperatures (i.e. hot climate zones).
  • Another preferred option is heating of appliances or thermally conditioned space with the heat pump.
  • heating can be crucial to the operation of appliances or for the personnel operating the appliances.
  • a heat driven heat pump can extremely efficiently provide heating.
  • a variety of fuels can be used in the power generator.
  • gaseous fuel are hydrogen, biologically produced gas, natural gas, compressed natural gas, liquefied natural gas, and propane.
  • Liquid fuels can also be used.
  • the system can also be adapted to solid fuels.
  • FIG. 6 schematically illustrates the system of the second preferred embodiment.
  • the system contains an electrical power generator 2 , a heat driven heat pump 4 , an appliance 6 , and a heat sink 8 .
  • the electrical power generator 2 can be a solid oxide fuel cell. It can also be a solid oxide fuel cell combined with a gas turbine. Other power generators, such as molten carbonate fuel cells, which also provide high temperature heat in addition to electrical power, can also be used.
  • the heat driven heat pump 4 can be an absorbtion chiller, such as a LiBr-Water or an ammonia-water heat pump. Heat driven heat pumps use high temperature heat to provide cooling (i.e. absorb heat at a low temperature), and reject heat at an intermediate temperature.
  • adsorption heat pumps Another class of heat driven heat pumps suitable for this embodiment is adsorption heat pumps.
  • the refrigerant which is usually a gas
  • Adsorption and desorption of the refrigerant on/from the solid provide pressurization of the refrigerant.
  • High pressure desorption of the refrigerant is accomplished using high temperature heat.
  • heat is rejected and in the low pressure portion heat is absorbed.
  • Adsorption heat pumps can be realized as solid state devices without the need to handle liquids. This can be advantageous for example in environments where handling of the liquids commonly involved in absorption heat pumps is too hazardous.
  • Environmentally friendly gases/vapors can be used in the adsorption heat pump.
  • the appliance 6 is a device that consumes electrical power for any purpose and generates heat (appliance cooling load), mostly as a parasitic loss, which needs to be removed.
  • appliance cooling load mostly as a parasitic loss, which needs to be removed.
  • One preferred example for this appliance is a computer or a cluster of computers co-located in a data center.
  • a heat sink 8 for the system can be a large body of solid, liquid or gas.
  • the heat sink can comprise, a cooling tower, ambient atmospheric air, soil, or a stream of water.
  • the energys exchanged between the subsystems can be transferred using electrical wire, but other electrical power transfer mechanisms can also be used.
  • the high temperature heat 10 is generated by the electrical power generator 2 and consumed by the heat driven heat pump 4 .
  • the high temperature heat 10 can be transported with a pumped fluid loop, such as a liquid loop, in which the fluid absorbs heat in or near the electrical power generator 2 and releases heat to the heat driven heat pump 4 .
  • this heat transfer can be accomplished by any heat transfer mechanism (i.e. conduction, convection, radiation, or any combination thereof).
  • the cooling loop can also consist of gas or vapor coolant and/ or solid beds.
  • the appliance cooling load 14 is the amount of heat generated by the appliance 6 , which needs to be removed by the heat pump 4 .
  • Heat is absorbed at or near the appliance 6 and transported to the heat driven heat pump 4 .
  • a liquid pumped loop or a stream of gas can be used to absorb the cooling load 14 from the appliance 6 and transport it to the heat driven heat pump 4 .
  • the moderate temperature heat 16 is the heat transferred from the heat driven heat pump 4 to the heat sink 8 .
  • convection, conduction, radiation, or any combination of these heat transfer mechanisms can be used to transport this heat.
  • One possible implementation is atmospheric air blown through a heat exchanger inside the heat driven heat pump and released back to ambient. All three heat transfers ( 10 , 14 , 16 ) can be realized with a single or multiple heat streams.
  • the moderate temperature heat 16 from the heat driven heat pump 4 to the heat sink 8 is commonly realized with two transport loops.
  • An example for the heat transfer loop from the heat driven heat pump 4 to the heat sink 8 is a pumped loop with tubes wrapped around the part of the heat driven heat pump 4 that requires cooling and coils of tubes buried in the soil.
  • Another example is a blower sucking in ambient air, blowing it over the surface that needs to be cooled and a conduit releasing the warm air back to ambient.
  • the subsystem formed by the electrical power generator 2 and the heat driven heat pump 4 is illustrated in FIG. 7 for the case where a high temperature fuel cell is used as the electrical power generator 2 .
  • the fuel cell 68 is preferably a high temperature fuel cell, such as a solid oxide fuel cell.
  • Fuel is delivered to the fuel cell with the help of a fuel blower 18 , which can also be a compressor.
  • a fuel blower 18 For liquid fuels, the blower 18 is replaced by a pump.
  • An optional fuel preconditioner 104 preprocesses the fuel. For example this device can remove contaminants detrimental to the function of the power generator, such as sulfur. Another possible function for the fuel preconditioner 104 is prereformation and/ or reformation.
  • the fuel preheater 22 brings the fuel to fuel cell operating temperature.
  • This preheater can be external to or an integral part of the fuel cell 68 . It can be contained in one single or multiple devices.
  • the fuel preheater 22 evaporates the liquid fuel.
  • the fuel preheater 22 can be a finned heat exchanger.
  • a fuel preconditioner 104 can also be implemented after the fuel preheater 22 or integrated with the fuel preheater 22 , or integral to fuel cell 68 .
  • the fuel preheat 54 is the heat required raise the temperature of the input fuel to the fuel cell operating temperature.
  • the fuel intake conduit 34 provides a path for the fuel from the fuel blower 18 to the fuel preheater 22 . It may or may not have an intermediate fuel preconditioner 104 .
  • the fuel delivery conduit 36 provides a path for the fuel from the fuel preheater 22 to the fuel cell 68 .
  • the oxidizer blower 20 drives air or any other suitable oxidizer toward the fuel cell 68 .
  • the oxidizer intake conduit 42 provides a transport path for the oxidizer between the oxidizer blower 20 and the oxidizer preheater 24 .
  • An optional oxidizer preconditioner 106 preprocesses the oxidizer flow. Examples of the preconditioner 106 include filters, and oxygen enrichment devices.
  • the preconditioner heat 11 A is heat required to operate this optional device.
  • One example for one component of the preconditioner 106 is an oxygen enrichment device utilizing temperature swing adsorption, as described in the first preferred embodiment.
  • the oxidizer preconditioner 106 can also be installed upstream of the oxidizer blower 20 .
  • the oxidizer preheater 24 brings the input oxidizer to fuel cell operating temperature using the oxidizer preheat 62 .
  • the oxidizer preheater 24 can be contained in single or multiple devices.
  • the oxidizer is partially preheated in oxidizer preheater 24 and picks up additional heat inside the fuel cell 68 , thereby cooling the fuel cell 68 .
  • One example for the oxidizer preheater 24 is a finned heat exchanger.
  • the oxidizer delivery conduit 44 transports the oxidizer from the oxidizer preheater 24 to the fuel cell 68 .
  • the fuel and the oxidizer are electrochemically reacted. This reaction produces electrical energy 12 and high temperature heat.
  • the fuel cell high temperature heat 58 represents the part of the heat generated by the fuel cell which is harnessed for further use and not removed by the exhaust or the depleted oxidizer. Not all of the heat generated by the fuel cell can be harnessed and transported to other devices.
  • the fuel cell high temperature heat 58 can be utilized for various purposes. This heat can be used for the fuel preheat 54 , the oxidizer preheat 62 , preconditioner heat 11 A, or the heat driven heat pump high temperature input heat 10 .
  • the fuel cell high temperature heat 58 can be directed to any combination of these heat consumers ( 10 , 54 , 62 , 11 A).
  • One possibility for harnessing the fuel cell high temperature heat 58 is a gas cooling loop, separate from the oxidizer flow loop to the fuel cell.
  • the fuel cell outlet conduits 38 and 46 transport the electrochemical reaction products. If the fuel cell 68 is a solid oxide fuel cell, then the exhaust conduit 38 transports reacted fuel and the outlet oxidizer conduit 46 transports oxygen depleted oxidizer.
  • the fuel outlet cooler 28 extracts the exhaust cooling heat 56 from the exhaust stream.
  • the fuel outlet cooler 28 can be one or multiple devices and can be partly or fully integrated with the fuel cell 68 .
  • One example for the fuel outlet cooler 28 is a finned heat exchanger.
  • the exhaust cooling heat 56 can be used for the fuel preheat 54 , the oxidizer preheat 62 , preconditioner heat 11 A, or the heat driven heat pump high temperature input heat 10 .
  • the exhaust cooling heat 56 can be directed to any combination of these heat consumers ( 10 , 54 , 62 , 11 A).
  • the oxidizer outlet cooler 26 extracts the oxidizer cooling heat 60 from the outlet oxidizer stream.
  • the oxidizer outlet cooler 26 can be one or multiple devices and can be partly or fully integrated with the fuel cell 68 .
  • One example for the oxidizer outlet cooler is a finned heat exchanger.
  • the oxidizer cooling heat 60 can be used for the fuel preheat 54 , the oxidizer preheat 62 , preconditioner heat 11 A, or the heat driven heat pump high temperature input heat 10 .
  • the oxidizer cooling heat 60 can be directed to any combination of these heat consumers ( 10 , 54 , 62 , 11 A).
  • the fuel outlet (i.e., exhaust) conduit 38 and the oxidizer outlet (i.e., exhaust) conduit 46 deliver fuel exhaust and oxygen depleted oxidizer to the optional burner 30 .
  • these two gas streams are chemically reacted, generating the burner high temperature heat 48 .
  • the chemical reaction can be initiated by an optional catalyst material.
  • the burner high temperature heat 48 can be provided to the fuel preheat 54 , the oxidizer preheat 62 , preconditioner heat 11 A, or the heat driven heat pump high temperature input heat 10 .
  • the burner high temperature heat 48 can be directed to any combination of these heat consumers ( 10 , 54 , 62 , 11 A).
  • One preferred example of transport of the burner high temperature heat 48 is direct integration of the burner with the consumer (i.e. heat transfer by conduction to the consumer). Another preferred example for this heat transport is a pumped fluid loop.
  • the burner exhaust conduit 50 transports the reaction products from the burner 30 to the optional burner exhaust heat exchanger 32 .
  • the burner exhaust heat 64 is extracted from the burner reaction products.
  • One example for the burner exhaust heat exchanger 32 is a finned heat exchanger.
  • the burner exhaust heat 64 can be provided to the fuel preheat 54 , the oxidizer preheat 62 , preconditioner heat 11 A, or the heat driven heat pump high temperature input heat 10 .
  • the burner exhaust heat 64 can be directed to any combination of these heat consumers ( 10 , 54 , 62 , 11 A).
  • the burner heat exchanger exhaust conduit 102 transports the burner exhaust out of the system (preferably vented to ambient or into an exhaust post-processor).
  • the heat driven heat pump 4 is driven by the high temperature heat 10 . After using heat from the high temperature heat 10 the heat driven heat pump 4 vents one heat stream in the heat pump low-temperature outflow 16 A.
  • the appliance cooling load 14 from appliance 6 is removed by the cooling stream 16 B.
  • the high temperature heat 10 can be provided by the fuel cell high temperature heat 58 , the exhaust cooling heat 56 , the oxidizer cooling heat 60 , the burner high temperature heat 48 , or the burner exhaust heat 64 .
  • the high temperature heat 10 can also be provided by any combination of these heat sources ( 48 , 56 , 58 , 60 , 64 ).
  • One preferred implementation for the appliance cooling load 14 and the heat 16 B is ambient air driven by a blower into the heat driven heat pump 4 , cooled below ambient temperature in the heat driven heat pump, and then directed to the appliance that requires cooling. At the appliance the cool air picks up the cooling load 14 and is heated. The heated air is vented back to ambient.
  • FIG. 8A One preferred embodiment of the system shown in FIG. 7 is presented in FIG. 8A.
  • the system shown in FIG. 8A follows the same outline presented for FIG. 7.
  • FIG. 8A includes one preferred routing of the heat streams shown in FIG. 7.
  • the fuel preheat 54 is provided by the fuel exhaust cooling heat 56 .
  • the fuel can pick up additional heat in the fuel cell.
  • the heat transfer from exhaust cooling heat 56 to fuel preheat 54 can be realized in a heat exchanger, for example a finned heat exchanger.
  • a heat exchanger for example a finned heat exchanger.
  • This configuration is to combine heat exchangers 22 and 28 as a single component.
  • water vapor can be transferred from the exhaust to the input fuel. This water transport can be integrated into a heat exchanger or it can be realized with a separate device.
  • the oxidizer preheat 62 is provided partly by the oxidizer exhaust cooling heat 60 .
  • the remainder of the heat needed to bring the oxidizer to fuel cell operating temperature is absorbed in the fuel cell, thereby removing all of the high temperature heat from the fuel cell without an additional heat transfer loop.
  • the heat transfer from oxidizer exhaust cooling heat 60 to oxidizer preheat 62 can be realized in a heat exchanger, for example a finned heat exchanger.
  • One example of this configuration is to combine heat exchangers 24 and 26 as a single component.
  • the burner high temperature heat 48 is not immediately extracted. Instead, it is extracted together with burner exhaust heat 64 .
  • the burner exhaust heat 64 is directed to the high temperature heat 10 , which provides the necessary heat to actuate the heat driven heat pump 4 .
  • the heat transfer from the burner exhaust heat 64 to the heat driven heat pump 4 can be realized with a heat exchanger incorporated in the heat driven heat pump 4 .
  • the burner exhaust heat exchanger 32 is combined with the heat exchanger in the heat pump 4 to form a single component.
  • This heat exchanger can be a finned heat exchanger.
  • the cooling load 14 can be extracted from the appliance 6 by a cool air stream provided by the heat driven heat pump 4 , which is driven with a cooling air-blower 72 through cooling air inlet duct 74 directed to the appliance with a cooling air conduit 76 .
  • Table 1 presents an energy balance for a 100 kW electrical power system based on FIG. 8A.
  • the naming convention, where applicable, is consistent with FIG. 8A.
  • TABLE 1 typical range example item low high layout units DC electrical power output 12 0.005 100 0.1 [MW]
  • Fuel cell efficiency 62.5% fraction of heat of fuel oxidized in fuel cell, which is available as DC electrical power
  • FIG. 8B illustrates another preferred aspect of the second embodiment of this invention.
  • the system illustrated in FIG. 8B shows an alternative preferred routing of the heat streams shown in FIG. 7.
  • the system depicted in FIG. 8B is similar to the system depicted in FIG. 8A, with the exception that the oxidizer cooling heat 60 is provided to the heat exchanger 4 as the high temperature heat 10 , and the burner exhaust heat 64 is provided to the oxidizer preheater 24 as oxidizer preheat 62 .
  • the oxidizer outlet conduit 46 is provided into the heat exchanger of the heat pump 4 and then into the burner 30 , while the burner exhaust conduit 50 is provided into the burner exhaust heat exchanger 32 .
  • Both the heat transfer from the oxidizer cooling heat 60 to the high temperature heat 10 and the burner exhaust heat 64 to the oxidizer preheat 62 can be realized with heat exchangers.
  • the oxidizer preheater 24 and the burner exhaust heat exchanger 32 are combined as a single component and comprise portions of the same heat exchanger 24 / 32 .
  • the outlet oxidizer cooler 26 and the heat exchanger portion of the heat pump 4 are combined as a single component and comprise a portion of the same heat exchanger.
  • FIG. 8C illustrates another preferred aspect of the second embodiment of this invention.
  • the system illustrated in FIG. 8C shows an alternative preferred routing of the heat streams shown in FIG. 7.
  • the system depicted in FIG. 8C is similar to the system depicted in FIG. 8A, but differs by a cross-over of the exhaust fuel and oxidizer paths.
  • the fuel outlet conduit 38 is provided into the oxidizer outlet cooler 28
  • the oxidizer outlet conduit 46 is provided into the fuel outlet cooler 26 .
  • the exhaust cooling heat 56 is provided as oxidizer preheat 62
  • oxidizer cooling heat 60 is provided as fuel preheat 54 . Both heat transfers can be realized with heat exchangers.
  • the oxidizer preheater 24 and the fuel outlet cooler 28 are combined as a single component and comprise portions of the same heat exchanger 24 / 28 .
  • the outlet oxidizer cooler 26 and the fuel preheater 22 are combined as a single component and comprise a portion of the same heat exchanger 22 / 26 .
  • FIG. 9 shows another preferred embodiment of the system depicted in FIG. 6.
  • the main difference between FIG. 7 and FIG. 9 is the addition of a gas turbine driven electrical power generator.
  • the gas turbine can utilize the high temperature heat from the fuel cell to generate additional electrical energy and thereby further increase the electrical efficiency of the electrical power generator.
  • High temperature waste heat is still available to drive a heat driven heat pump and thereby form a complementary system, which can provide matched electrical power and cooling.
  • the increase of efficiency of the power generator implies that less high temperature heat per electrical power generated is available.
  • Such an embodiment is used preferentially when the electrical load requirements are greater than the cooling load requirements and there are no environmental and permitting issues against the use of gas turbines.
  • This embodiment can also be used with a heat driven heat pump of higher efficiency such as to complete the balance between the electrical and thermal loads in the system described above.
  • the fuel is compressed and transported into the system by the fuel compressor 80 .
  • a fuel compressor inlet conduit 82 delivers the fuel to the fuel compressor 80 .
  • a fuel pump can be used instead of the fuel compressor 80 .
  • An optional fuel preconditioner 104 preprocesses the fuel. For example this device can remove contaminants detrimental to the function of the power generator, such as sulfur. Another possible function for the fuel preconditioner 104 is prereformation or reformation.
  • the fuel preheater 22 brings the fuel to fuel cell operating temperature. If the fuel is provided as a liquid, the fuel is evaporated in the fuel preheater 22 . This preheater can be external to or an integral part of the fuel cell 68 . It can be contained in one single or multiple devices.
  • the fuel preheat 54 is the heat required to bring the fuel to fuel cell operating temperature.
  • the fuel intake conduit 34 provides a path for the fuel from the fuel compressor 80 to the fuel preheater 22 .
  • the fuel delivery conduit 36 provides a path for the fuel from the fuel preheater 22 to the fuel cell 68 .
  • the oxidizer compressor 84 drives air or any other suitable oxidizer to the fuel cell 68 .
  • the oxidizer compressor inlet conduit 86 delivers the oxidizer to the oxidizer compressor 84 .
  • An optional oxidizer preconditioner 106 preprocesses the oxidizer flow. Examples of the preconditioner 106 include filters, and oxygen enrichment devices.
  • the preconditioner heat 11 A is heat required to operate this optional device.
  • One example for one component of the preconditioner 106 is an oxygen enrichment device utilizing temperature swing adsorption.
  • the oxidizer preconditioner 106 can also be installed downstream of the oxidizer compressor 84 .
  • the oxidizer intake conduit 42 provides a transport path for the oxidizer between the oxidizer compressor 84 and the oxidizer preheater 24 .
  • the oxidizer preheater 24 brings the input oxidizer to fuel cell operating temperature using the oxidizer preheat 62 .
  • the oxidizer preheater 24 can be contained in a single or multiple devices. In one preferred embodiment, the oxidizer is partially preheated in oxidizer preheater 24 and picks up additional heat inside the fuel cell 68 , thereby cooling the fuel cell 68 .
  • the oxidizer delivery conduit 44 transports the oxidizer from the oxidizer preheater 24 to the fuel cell 68 .
  • the oxidizer outlet cooler 26 extracts the oxidizer cooling heat 60 from the outlet oxidizer stream.
  • the outlet oxidizer cooler 26 can be one or multiple devices and can be partly or fully integrated with the fuel cell 68 .
  • the fuel outlet cooler 28 extracts the exhaust cooling heat 56 from the exhaust stream.
  • the fuel outlet cooler 28 can be one or multiple devices and can be partly or fully integrated with the fuel cell 68 .
  • One example for the coolers 26 , 28 is a finned heat exchanger.
  • the fuel exhaust conduit 38 and the oxidizer outlet conduit 46 deliver fuel exhaust and oxygen depleted oxidizer to the optional burner 30 .
  • these two gas streams are chemically reacted, generating the burner high temperature heat 48 .
  • the burner high temperature heat 48 can be provided to the fuel preheat 54 , the oxidizer preheat 62 , the preconditioner heat 11 A, or the high temperature heat 10 .
  • the burner high temperature heat 48 can be directed to any combination of these heat consumers ( 10 , 11 A, 54 , 62 ).
  • the burner exhaust conduit 50 transports the reaction products from the burner 30 to the optional burner exhaust heat exchanger 32 .
  • the burner exhaust heat 64 is extracted from the burner reaction products.
  • the burner exhaust heat 64 can be provided to the fuel preheat 54 , the oxidizer preheat 62 , the preconditioner heat 11 A, or the high temperature heat 10 .
  • the burner exhaust heat 64 can be directed to any combination of these heat consumers ( 10 , 11 A, 54 , 62 ).
  • the turbine inlet conduit 88 transports the burner exhaust to the turbine 90 .
  • a mechanical coupling 92 transmits mechanical energy from the turbine 90 to the oxidizer compressor 84 , the fuel compressor 80 , and/or the electrical generator 94 . If desired, the compressors may be actuated by another source of mechanical energy and/or electrical power.
  • the electrical generator 94 generates additional electrical power 12 B.
  • the turbine outlet conduit 96 transports the turbine exhaust to the optional turbine exhaust heat exchanger 98 .
  • the turbine exhaust heat 100 A is extracted from the gas flow.
  • the turbine exhaust heat 100 A can be provided to the fuel preheat 54 , the oxidizer preheat 62 , the preconditioner heat 11 A, or the high temperature heat 10 .
  • the turbine exhaust heat 100 A can be directed to any combination of these heat consumers ( 10 , 11 A, 54 , 62 ).
  • the exhaust conduit 102 transports the exhaust gases out of the system (preferably vented to ambient or into an exhaust post-processor).
  • the heat driven heat pump 4 is driven by the high temperature heat 10 . After utilizing heat from the high temperature heat 10 , the heat driven heat pump 4 vents one heat stream in the moderate temperature heat 16 A.
  • the appliance cooling load 14 from appliance 6 is removed by the cooling stream 16 B.
  • the high temperature heat 10 can be provided by the fuel cell high temperature heat 58 , the exhaust cooling heat 56 , the oxidizer cooling heat 60 , the burner high temperature heat 48 , the burner exhaust heat 64 , or the turbine exhaust heat 100 A.
  • the high temperature heat 10 can also be provided by any combination of these heat sources ( 46 , 56 , 58 , 60 , 64 , 100 A).
  • FIG. 10A One preferred embodiment of the system shown in FIG. 9 is presented in FIG. 10A.
  • the system shown in FIG. 10A follows the same outline presented for FIG. 9.
  • FIG. 10A includes one preferred routing of the heat streams involved.
  • the fuel preheat 54 is provided by the exhaust cooling heat 56 .
  • the fuel can pick up additional heat in the fuel cell.
  • the heat transfer from exhaust cooling heat 56 to fuel preheat 54 can be realized in a heat exchanger, for example a finned heat exchanger 22 / 28 .
  • water vapor can be transferred from the exhaust to the input fuel. This water transport can be integrated into a heat exchanger or it can be realized with a separate device.
  • the oxidizer preheat 62 is provided partly by the oxidizer cooling heat 60 .
  • the remainder of the heat needed to bring the oxidizer to fuel cell operating temperature is absorbed in the fuel cell, thereby removing all of the high temperature heat from the fuel cell without an additional heat transfer loop.
  • the heat transfer from oxidizer cooling heat 60 to oxidizer preheat 62 can be realized in a heat exchanger, for example a finned heat exchanger 24 / 26 .
  • the burner high temperature heat 48 together with the high temperature heat from the fuel cell carried by the burner exhaust gas 64 is first used to drive the turbine 90 .
  • the remaining heat after the turbine is used as high temperature heat 10 to drive the heat driven heat pump 4 .
  • the heat transfer from the turbine exhaust heat 100 A to the heat driven heat pump 4 can be realized with a heat exchanger incorporated in the heat driven heat pump 4 .
  • This heat exchanger can be a finned heat exchanger.
  • the cooling load 14 can be absorbed from the appliance 6 by a cool air stream provided by the heat driven heat pump 4 , which is driven with a cooling air blower 72 through cooling air inlet duct 74 directed to the appliance with a cooling air conduit 76 .
  • FIG. 10B illustrates another preferred aspect of the second embodiment of this invention.
  • the system illustrated in FIG. 10B shows an alternative preferred routing of the oxidizer stream shown in FIGS. 9 and 10A.
  • the system depicted in FIG. 10B is similar to the system depicted in FIG. 10A, with the exception of the oxidizer routing.
  • the gas turbine 90 and the fuel cell 68 are fed with separate oxidizer streams.
  • An oxidizer blower 20 is used for the oxidizer supply for the fuel cell.
  • This blower can also be a compressor.
  • the compressor 84 delivers oxidizer to the burner 30 via conduit 45 A.
  • the unreacted fuel from the fuel cell is combusted in the burner.
  • the burner exhaust drives the turbine 90 .
  • the advantage of this system is that a higher oxygen content oxidizer is supplied to the burner. This improves the combustion process in the burner and subsequently improves the turbine operation.
  • FIG. 10C illustrates another preferred aspect of the second embodiment of this invention.
  • the system illustrated in FIG. 10C shows an alternative preferred routing of the heat streams shown in FIG. 9.
  • the system in FIG. 10C is differs from the system in FIG. 10A by the sequence of heat usage from the oxidizer.
  • the oxidizer leaving the fuel cell 68 first delivers the oxidizer cooling heat 60 to the high temperature input heat 10 in the heat pump 4 , and then enters the burner 30 .
  • the oxidizer preheat 62 is provided by the turbine exhaust heat 100 A.
  • the oxidizer preheater 24 and the turbine exhaust heat exchanger 98 are combined as a single component and comprise portions of the same heat exchanger 24 / 98 .
  • the outlet oxidizer cooler 26 and the heat exchanger portion of the heat pump 4 are combined as a single component and comprise a portion of the same heat exchanger.
  • FIG. 10C relates similarly to FIG. 10A as the system in FIG. 8B relates to the system in FIG. 8A.
  • the system in FIG. 10C can also incorporate the use of separate oxidizers for the fuel cell and the burner 30 , as shown in FIG. 10B. It may be advantageous to provide separate oxidizer streams for the fuel cell 68 and the turbine 90 .
  • FIG. 10D illustrates another preferred aspect of the second embodiment of this invention.
  • the system illustrated in FIG. 10D shows an alternative preferred routing of the heat streams shown in FIG. 9.
  • the system depicted in FIG. 10D is similar to the system depicted in FIG. 10A, but differs by the routing of the heat fluxes.
  • the fuel preheat 54 is provided by the turbine exhaust heat 100 A, while the high temperature heat 10 is provided by the fuel exhaust cooling heat 56 .
  • the turbine outlet conduit 96 is provided into the turbine exhaust heat exchanger 98
  • the fuel cell fuel outlet conduit 38 is provided into the heat exchanger portion of the heat pump 4 .
  • the turbine exhaust heat exchanger 98 and the fuel preheater 22 are combined as a single component and comprise portions of the same heat exchanger 22 / 98 .
  • the outlet fuel cooler 28 and the heat exchanger portion of the heat pump 4 are combined as a single component and comprise a portion of the same heat exchanger. This routing can be applied to any of the systems of FIGS. 10A, 10B and 10 C previously discussed.
  • FIGS. 6 to 10 D present the basic layouts of the components of the systems of the preferred aspects of the second embodiment. These components can also be combined in a large number of other ways not shown in these Figures. Any component or combination of components shown in one figure may be used in a system shown in any other figure. For example, the cross over of the fuel cell fuel and oxidizer exhaust paths shown in FIG. 8C can be applied to the systems shown in FIGS. 8A, 8B, 10 A, 10 B, 10 C, 10 D, as well as combinations of these systems.
  • the ceramic electrolyte 101 is corrugated, as shown in FIG. 11. While the whole electrolyte 101 is bent or corrugated, its major surfaces 103 , 105 are smooth or uniform. Thus, the electrolyte 101 has the same thickness along its length. However, the imaginary center line 107 running along the length of the electrolyte 101 significantly deviates from an imaginary straight line 109 . The anode 111 and cathode 113 are formed on the uniform surfaces 103 , 105 of the electrolyte 101 . Such a corrugated electrolyte 101 is difficult to manufacture and even more difficult to properly integrate in a fuel cell stack containing a plurality of fuel cells.
  • the present inventors have realized that if at least a portion of at least one surface of the electrolyte is made non-uniform, then several advantages may be realized.
  • the oxygen diffusion through an electrolyte in a solid oxide fuel cell proceeds between so-called “three phase boundaries.” These three phase boundaries are electrolyte grain boundary regions at the boundary of an electrode (i.e., cathode or anode) and electrolyte, as shown in FIG. 12. Diffusing oxygen makes up the third “phase.” If the active portions of one or both major surfaces of the electrolyte are made non-uniform, then the surface area between the electrolyte and the electrode contacting the non-uniform surface is increased.
  • the “active portion” of the electrolyte is the area between the electrodes that generates the electric current.
  • the peripheral portion of the electrolyte is used for attaching the electrolyte to the fuel cell stack and may contain fuel and oxygen passages.
  • the increased surface area results in more three phase boundary regions, which allows more oxygen to diffuse through the electrolyte. This increases the power density (i.e., watts per cm 2 ) of the fuel cell and decreases the cost per watt of the fuel cell.
  • FIG. 13 illustrates a solid oxide fuel cell 200 containing a ceramic electrolyte 201 having at least one non-uniform surface portion, according to a first preferred aspect of the third embodiment.
  • the at least one non-uniform surface in the first preferred aspect is a textured surface.
  • two opposing major surfaces 203 , 205 are textured.
  • a textured surface 203 , 205 contains a plurality of protrusions (i.e., bumps, peaks, etc.) 206 having a height 208 that is 5% or less, preferably 1% or less of an average electrolyte thickness 209 .
  • the height and width of the protrusions 206 is exaggerated in FIG. 13 for clarity.
  • the protrusions 206 may have any desired shape, such as rectangular, polygonal, triangular, pyramidal, semi-spherical or any irregular shape.
  • the active portions 210 of the opposing major surfaces 203 , 205 are textured, while the peripheral portions 202 of the surfaces 203 , 205 are not textured.
  • the entire major surfaces 203 , 205 may be textured.
  • texturing the peripheral portions can increase the seal integrity and/ or reduce the “non-active” peripheral area of the fuel cell.
  • the electrolyte shown in FIG. 13 is substantially flat.
  • the imaginary center line 207 running along the length of the electrolyte 201 does not significantly deviate from an imaginary straight line. While the whole electrolyte 201 is substantially flat, its major opposing surfaces 203 , 205 are non-uniform and textured.
  • the anode 211 and cathode 213 are formed on the textured surfaces 203 , 205 of the electrolyte 201 .
  • the substantially flat electrolyte is advantageous because it is easier to manufacture, because it is easier to integrate into a fuel cell stack and because it is more durable than a corrugated electrolyte. However, if desired, the textured surface(s) may be located on a non-flat or corrugated electrolyte.
  • the electrolyte, anode and cathode may be made of any appropriate materials.
  • the electrolyte comprises a yttria stabilized zirconia (YSZ) ceramic.
  • the cathode preferably comprises a Perovskite ceramic having a general formula ABO 3 , such as LaSrMnO 3 (“LSM”).
  • LSM LaSrMnO 3
  • the anode preferably comprises a metal, such as Ni, or a metal containing cermet, such as a Ni—YSZ or Cu—YSZ cermet. Other suitable materials may be used if desired.
  • the non-uniform surface of the electrolyte may be formed by any suitable method.
  • the non-uniform surface is made by providing a ceramic green sheet and patterning at least a portion of at least one surface of the green sheet to form at least a non-uniform portion of the at least one surface.
  • the green sheet may then be sintered (i.e., fired or annealed at a high temperature) to form the ceramic electrolyte.
  • the term “green sheet” includes a green tape or a sheet of finite size. Preferably both sides of the green sheet are patterned to form two opposing non-uniform surface portions of the green sheet.
  • FIG. 14 illustrates a prior art composite electrolyte
  • FIGS. 15 and 16 illustrate a composite electrolyte with a textured interface according to the third preferred embodiement.
  • YSZ yttria stabilized zirconia
  • One example for composite electrolyte is a samaria-doped ceria (SDC) electrolyte coated with YSZ on one or both sides. SDC has the advantage over YSZ to provide higher ionic conductivity.
  • SDC samaria-doped ceria
  • SDC is limited by its ability to withstand low oxygen partial pressures. At low oxygen partial pressures SDC can be reduced, lose its ionic conductivity in part or in whole and thereby cause a critical failure in a solid oxide fuel cell.
  • YSZ has a lower ionic conductivity, which implies higher electrical losses within this material, but it can withstand lower oxygen partial pressures compared to SDC.
  • SDC displays electron conductivity at elevated temperatures, which is detrimental to the performance of a fuel cell.
  • a layer of YSZ next to SDC can effectively suppress electron conduction, since YSZ is a very weak electron conductor.
  • FIG. 14 shows a prior art YSZ electrolyte 300 , which is coated or laminated with a layer of SDC 305 .
  • SDC SDC
  • One example is to use the SDC on the cathode side of the solid oxide fuel cell, which is not exposed to the reacting fuel, and thereby not exposed to low oxygen partial pressure, while the YSZ is used on the anode side.
  • FIG. 15 shows a cross section of a composite electrolyte with a textured internal interface.
  • a textured layer of SDC 315 is attached to a layer of YSZ 310 .
  • the combination of YSZ and SDC is one example where a textured interface can be used. Other material combination can also be used with textured interfaces.
  • the composite electrolyte can consist of two layers as shown in FIG. 15 or of three or more layers 310 , 315 , 320 with at least one, and preferably more than one textured interface 303 , 305 as shown in FIG. 16.
  • Textured interfaces can be formed by any suitable method.
  • One method is the lamination of two textured matching surfaces.
  • Another method is the application of the second layer onto a textured surface of the first material, for example by tape casting or by screen printing.
  • the SDC is provided as a mechanically supporting substrate with a thickness of about 50 to 200 micrometers, preferably about 100 micrometers and the YSZ is deposited on the substrate as a thin protective layer of about 10 to 50 micrometers, preferably about 20 micrometers.
  • the surface texture can have a thickness of about 10 micrometers.
  • texturing on larger and smaller length scales is also possible.
  • the textured internal interfaces (i.e., interface surfaces) illustrated in FIGS. 15 and 16 can be formed on composite electrolytes also having textured outer surfaces 203 , 205 (i.e., surfaces that contact the electrodes).
  • textured outer surfaces 203 , 205 i.e., surfaces that contact the electrodes.
  • One or both of the outer composite electrolyte surfaces can be textured.
  • Additional layers that offer superior mechanical, thermal, and/or electrical properties may be added to composite or single layer electrolytes to provide improved superior mechanical, thermal, and/or electrical properties compared to single layer electrolytes.
  • multiple layers of functionally graded electrodes may be provided on single layer or composite electrolytes.
  • the textured surface(s) 203 , 205 illustrated in FIGS. 13 and 15 may be textured by several different methods.
  • the textured surface is formed by laser ablating the green sheet, following by sintering the green sheet. Any suitable laser ablation method and apparatus may be used to texture the green sheet.
  • a schematic illustration of a laser ablation apparatus 250 suitable for texturing the green sheet surface is shown in FIG. 17.
  • a laser source 251 directs a laser beam 253 at a reflective mirror 255 .
  • the mirror 255 directs the beam 253 through a focusing lens 257 onto the green sheet (such as an unfired electrolyte tape) 261 located on the precision XYZ table 259 .
  • Any laser source 251 which has sufficient power to ablate the green sheet 261 may be used.
  • excimer or YAG lasers may be used as the laser source 251 .
  • the laser beam 253 is scanned over the surface of the green sheet 261 by moving the XYZ table and/or by moving the mirror 255 .
  • the laser beam power may be varied during the scanning to achieve a non-uniform textured green sheet surface.
  • the laser source 251 may be periodically turned on and off, or it may be attenuated by an attenuator (not shown) to vary the laser beam power.
  • the XYZ table may be moved up and down during the scanning of the beam 253 to vary- the beam power that impinges on the green sheet 261 .
  • the laser beam 253 ablates (i.e., removes or roughens) a portion of a top surface of the green sheet 261 to leave a textured surface.
  • the textured green sheet is then sintered or fired to form the ceramic electrolyt
  • the textured surface of the green sheet may be formed by photolithography methods that are used in semiconductor manufacturing.
  • an etching mask 271 is formed on the green sheet 261 .
  • the etching mask 271 may comprise a photoresist layer that has been exposed through an exposure mask and developed.
  • the unmasked portions 273 of the green sheet are etched to form recesses in the top surface of the green sheet.
  • the masked portions 275 of the green sheet are protected from etching by the mask 271 , and remain as protrusions 275 between the recesses 273 .
  • the protrusions 275 and recesses 273 form a textured surface.
  • the photoresist mask 271 is removed after etching by a conventional selective removal process, such as ashing. Any etching gas or liquid that preferentially etches the green sheet material to the mask material may be used. As shown in FIG. 18, an anisotropic etching medium was used to form recesses 273 with straight sidewalls. This results in rectangular protrusions 275 between the recesses. Alternatively, an isotropic etching medium may be used to form recesses 273 with outwardly sloped walls. This results is trapezoidal or pyramidal protrusions 275 between the recesses.
  • the mask may comprise materials other than photoresist. In one example, other photosensitive layers may be used. Alternatively, a so-called “hard mask” may be used as a mask to etch the green sheet. For example, as shown in FIG. 19, a hard mask layer 281 is deposited on the green sheet 261 .
  • the hard mask layer 281 may be any material which resists being etched by an etching medium to a higher degree than the green sheet 261 .
  • the hard mask layer may be any suitable metal, ceramic, semiconductor or insulator.
  • a photoresist mask 271 is formed, exposed and developed over the hard mask layer 281 . The hard mask layer 281 is then etched using the photoresist as a mask.
  • the green sheet 261 is etched to form a textured surface containing a plurality of recesses 273 and protrusions 275 using the hard mask 281 as a mask.
  • the photoresist mask 271 may be removed before or after the green sheet is etched.
  • the hard mask 281 is removed after the green sheet 261 is textured by a selective etching medium which removes the hard mask 281 but does not etch the green sheet 261 .
  • the mask may comprise a plurality of particles. As shown in FIG. 20, a plurality of discontinuous particles 291 are formed on the surface of the green sheet 261 .
  • the particles 291 may be any material which resists being etched by an etching medium to a higher degree than the green sheet 261 .
  • the particles may be any suitable metal, ceramic (such as titania or alumina), semiconductor (such as polysilicon or silicon carbide) or insulator.
  • the particles may be formed by any particle deposition method, such as spray coating, dip coating, ink jet deposition, sputtering or chemical vapor deposition.
  • the portions 273 of the green sheet 261 that are not covered by the particles 291 are etched to form recesses in the top surface of the green sheet.
  • the covered portions 275 of the green sheet are protected from etching by the particles 291 , and remain as protrusions between the recesses 273 .
  • the protrusions 275 and recesses 273 form a textured surface.
  • the particles 291 are removed after the green sheet 261 is textured by a selective etching medium which removes the particles 291 but does not etch the green sheet 261 .
  • the particles 291 may be formed by etching a textured layer 293 on the green sheet 261 .
  • a layer 293 with a rough or textured surface is deposited on the green sheet 261 .
  • the textured surface of layer 293 contains protrusions 295 .
  • This layer 293 may be any material with has a rough surface, such as hemispherical grain polysilicon, ceramic, insulator or metal.
  • Layer 293 is then anisotropically etched until only the protrusions 295 remain on the surface of the green sheet 261 , as shown in FIG. 22.
  • the remaining protrusions 295 appear as a plurality of particles on the green sheet 261 .
  • the green sheet 261 is then etched using the protrusions 295 as a mask.
  • the textured surface is formed without a mask.
  • an etching medium such as an etching liquid, which preferentially attacks the grain boundaries 297 of the green sheet 261 is applied to an upper surface of the green sheet.
  • the etching medium selectively etches the grain boundaries 297 of the green sheet to form recesses 273 .
  • the regions of the green sheet 261 between the grain boundaries 297 are not etched or are etched to a lesser degree and remain as protrusions 275 , as shown in FIG. 23.
  • a textured surface comprising protrusions 275 and recesses 273 is formed without a mask.
  • the textured surface is formed by embossing.
  • a body 298 i.e., a press, etc.
  • the lower surface 299 of body 298 has a higher hardness than the green sheet 261 .
  • the body 298 may be a ceramic, insulator or a metal body with a suitable hardness to emboss the green sheet.
  • the embossing step leaves impressions or recesses in the green sheet 261 to form the textured surface in the green sheet. It should be noted that both sides of the green sheet 261 may be textured by the methods described above.
  • the textured surface is formed by building the ridges on a flat green tape. This can be done using a cladding process or by a powder/slurry spray process, where the powder and/or slurry is made of the same material as the green tape.
  • the green tape is prepared by tape casting.
  • a raw ceramic powder for example YSZ
  • solvents for example YSZ
  • binders for example YSZ
  • plastisizers for example YSZ
  • defloculants for example YSZ
  • the slurry is applied to a mylar film (“carrier”) and spread uniformly with a blade, which is dragged along the length of the carrier with a precisely adjusted gap between the blade and the carrier.
  • carrier mylar film
  • this process is run continuously by moving the carrier under a static blade and applying slurry to the carrier upstream of the blade.
  • the thickness of the green tape can range between about 20 micrometer and 10,000 micrometers, preferably about 50 to 1,000 micrometers.
  • the amplitude of the surface texture can vary between 5 micrometers and 1000 micrometers, preferably about 10 to 30 micrometers.
  • the surface texturing can also be applied to electrolytes formed by other methods, such as electrolytes formed by extrusion.
  • the texturing is not limited to electrolytes with planar geometries, but can also be applied to electrolytes with non-planar geometries.
  • the inventors have realized that the quality, robustness and environmental endurance of the solid oxide fuel cell can be improved by using an environment tolerant anode catalyst.
  • an environment tolerant anode catalyst For example, when feeding a fuel contaminated with sulfur, a solid oxide fuel cell anode catalyst that is tolerant to sulfur may be used.
  • a fuel cell anode catalyst that is tolerant to fuel starvation may be used.
  • the low temperature acid fuel cell is fundamentally different than the solid oxide fuel cell.
  • the ionized fuel In the acid fuel cell, the ionized fuel must pass through the electrolyte to be reduced at the cathode by an oxidant.
  • the fuel ion in this case is the hydrogen proton.
  • sulfur is present in the fuel, the ionization reaction at the anode is slowed.
  • the mechanism for this occurrence is not well known, but it is believed to be related to the masking of the catalyst with the sulfur adsorbed onto the active catalytic material.
  • the solid oxide fuel cell it is the oxidant oxygen anion that must pass through the electrolyte to oxidize the fuel.
  • the sulfur contamination of the fuel creates no hindrance for the ionization of the oxygen or its transport through the electrolyte.
  • FIG. 25 compares the functionality of the solid oxide fuel cell 400 and an acid fuel cell 410 .
  • the electrolyte 411 can be a membrane such as duPont's Nafion® or an inert matrix filled with phosphoric acid. Other acids may be used, but the Nafion® and matrix phosphoric acids are the more frequently used.
  • the cathode electrode 412 is attached to or placed against the electrolyte 411 and usually contains platinum metal as the ionization catalyst for the air oxidant 414 .
  • the platinum is often a finely divided platinum black bonded with Teflon or platinum supported on carbon and bonded with Nafion® ionomer.
  • the anode electrode 413 is also attached to or placed against the electrolyte 411 and is similar to the cathode electrode 412 , except that ruthenium, rhodium, or other metals are frequently added to the platinum to make the anode electrode 413 more tolerant to CO gas in the hydrogen fuel 415 .
  • the source of hydrogen fuel 415 is a reformed hydrocarbon fuel. Usually the fuel source is scrubbed of sulfur down to the parts per billion (PPB) range. Otherwise, the anode electrode 413 functionality is significantly reduced. Additionally, the reformed fuel is processed to reduce the CO volume content in the hydrogen fuel 415 to less than 50 parts per million (PPM) to minimize the poisoning effect on the electrode.
  • the hydrogen fuel 415 is ionized at anode electrode 413 producing hydrogen protons.
  • the protons then pass through the membrane 411 by the gradient created by the combination with oxygen anions produced on the cathode electrode 412 from air oxidant 414 to produce product water 412 .
  • the electrolyte 401 is preferably yttria-stabilized zirconia (YSZ), although other ceramic oxides, such as ceria are sometimes used together with or instead of YSZ.
  • a preferred cathode electrode 402 is made from a 50:50 mixture of YSZ and La 0.8 Sr 0.2 MnO 3 (LSM). Other materials may be used if desired.
  • the cathode electrode 402 is attached to or placed against the electrolyte 401 and ionizes the oxygen in the air oxidant 404 .
  • the oxygen anions pass through the electrolyte 401 by the gradient created by the consumption of the anions by combination with fuel ions.
  • the anode electrode 403 is a often a ceramic-metallic (cermet) of Ni and YSZ, while Cu is sometimes used instead of Ni.
  • Hydrogen fuel 405 is ionized at the anode electrode 403 and combines with the oxygen anions to form water.
  • Ni/YSZ anode electrode performs very well with pure hydrogen fuel, but when attempting to internally reform a hydrocarbon fuel into a hydrogen rich fuel stream the Ni/YSZ anode electrode has shortcomings related to carbon formation and sulfur poisoning.
  • water i.e., water vapor
  • the fuel cell product water is generated within the anode electrode, even more water must be added to the fuel to prevent the carbon formation. This extra water must be introduced with the incoming fuel, which complicates the operation of the fuel cell.
  • the prior art Ni/YSZ electrode cannot tolerate even the 10 ppm sulfur normally found in natural gas. Thus, expensive sulfur scrubbing equipment is often used to reduce the sulfur content of the fuel, which increases the cost of the electricity generation.
  • sulfur tolerant compounds are used in combination with or instead of Ni in the anode cermet of a solid oxide fuel cell.
  • the sulfur tolerant compounds include any compounds which increase the anode tolerance to sulfur in the fuel stream. While the inventors do not want to be bound by any theory of operation of the sulfur tolerant compounds, it is believed that the sulfur tolerant compounds prevent or reduce the formation of sulfur on the anode.
  • the preferred sulfur tolerant compounds include MoWO x , RuO 2 , WO x , such as WO 2.5 , MOS 2 , WS 2 , and PtS x . Some compounds, such as WO x are also CO tolerant.
  • Less preferred compounds include sulfur tolerant catalysts usable in a molten carbonate fuel cell, such as Cr 2 O 3 , FeO, Fe 2 O 3 , Fe 3 O 4 , Al 2 O 3 , LiAlO 2 , LiCrO 2 , MO 2 , MO 3 and WO 3 , as described in U.S. Pat. No. 4,925,745, incorporated herein by reference.
  • the anode cermet comprises the ceramic, such as (YSZ), and a catalyst.
  • the catalyst preferably comprises 10 to 90 weight % Ni or Cu and 10 to 90 weight percent of the sulfur tolerant compound. Most preferably, the catalyst comprises 30 to 70 weight % Ni or Cu and 30 to 70 weight percent of the sulfur tolerant compound.
  • some sulfur tolerant compounds, such as PtS x may be used without Ni or Cu and comprise 100% of the catalyst.
  • These sulfur tolerant catalyst compounds in combination with or replacing the Ni in the anode electrode cermet provide an increased tolerance to sulfur in the fuel.
  • the sulfur tolerant catalyst allows the solid oxide fuel cell to be used with a hydrogen fuel source containing contaminate levels of sulfur compounds, such as more than 10 ppb, for example more than 100 ppb.
  • the three elements that combine in a non-obvious manner to achieve this tolerance include: weak tolerance of the Ni cermet to sulfur, uninhibited availability of an oxidant within the anode electrode, and elevated operational temperature.
  • the environmental tolerant anode catalyst comprises a fuel starvation tolerant catalyst.
  • the reactants are independently flow controlled.
  • the cathode airflow is generally controlled to supply sufficient oxygen for the cathode reaction and to remove the waste heat from the fuel cell reaction.
  • airflow 1.5 to 2.5 times the stoichiometric requirements is ample to satisfy the cathode reaction.
  • Heat removal will generally require much more airflow than that required in satisfying the cathode reaction and therefore, there is no reasonable concern that a cell will become oxygen starved.
  • the fuel is flow controlled only to support the anode reaction.
  • the fuel flow is generally set at about 1.2 times the stoichiometric requirements of the anode in order to maintain a high level of fuel utilization. This high level of fuel utilization is required to obtain a high overall system efficiency.
  • FIG. 26 shows the functionality of the solid oxide fuel cell 500 in the normal anode and normal cathode reaction modes and the anode reaction in the fuel starved mode.
  • the electrolyte 501 is usually yttria-stabilized zirconia (YSZ), although other ceramic oxides such as ceria are sometimes used.
  • the typical cathode electrode 502 is made from a 50:50 mixture of YSZ and La 0.8 Sr 0.2 MnO 3 (LSM). Other materials may be used if desired.
  • the cathode electrode 502 is attached to or placed against the electrolyte 501 and ionizes the oxygen in the air oxidant 504 .
  • the oxygen anions pass through the electrolyte 501 by the gradient created by the consumption of the anions by combination with fuel ions.
  • a prior art anode electrode 503 is configured with a ceramic-metallic (cermet) of Ni and YSZ. Alternately, Cu is sometimes used as the metal in the cermet for the anode electrode. Hydrogen/CO fuel 505 is ionized at the anode electrode 503 and combines with the oxygen anions to form water and CO 2 .
  • cermet ceramic-metallic
  • Hydrogen/CO fuel 505 is ionized at the anode electrode 503 and combines with the oxygen anions to form water and CO 2 .
  • the present inventors have realized that if a metal which forms a reversible oxide without damage to the metal is added to the anode, then the anode is rendered fuel starvation tolerant.
  • a metal forms an oxide when oxidized and reverts back to a pure metal without significant damage when the oxide is reduced by the fuel reaction at the anode.
  • the fuel starvation tolerant compound include platinum group metals, such as platinum, palladium, rhodium, iridium, osmium and ruthenium. Low temperature water electrolysis shows that platinum metal electrodes can be oxidized and reduced without damage.
  • Other catalytic materials or additives that display this characteristic include ruthenium and tungsten at various oxide levels. The use of these metals/oxides in various ratios provides the tolerance to the oxidative anode conditions during fuel starvation.
  • the anode 503 comprises a cermet which includes the ceramic, such as (YSZ), and a fuel starvation tolerant catalyst.
  • the catalyst preferably comprises 10 to 90 weight % Ni or Cu and 10 to 90 weight percent of the fuel starvation tolerant material.
  • the catalyst comprises 30 to 70 weight % Ni or Cu and 30 to 70 weight percent of the fuel starvation tolerant material.
  • the fuel starvation tolerant material oxidizes preferentially to Ni during fuel starvation.
  • some fuel starvation tolerant materials, such as Pt may be used without Ni or Cu and comprise 100% of the catalyst.
  • the anode comprises an environmental tolerant catalyst which is both a sulfur tolerant catalyst and a fuel starvation tolerant catalyst.
  • the anode may contain a combination of similarly based fuel starvation and sulfur tolerant materials, such as Pt and PtS x , Ru and RuO 2 , and W and WO x .
  • the anode may contain a combination of dissimilar catalysts, such as a Pt—WO x or Pt—HXWO 3 as disclosed in U.S. Pat. No. 5,922,488 incorporated herein by reference in its entirety.
  • any combination of the sulfur tolerant and fuel starvation tolerant materials described above may be selected for the anode composition.
  • the anode 503 comprises a cermet which includes the ceramic, such as (YSZ), and a environment tolerant catalyst.
  • the catalyst preferably comprises 10 to 90 weight % Ni or Cu, 5 to 45 weight percent of the sulfur tolerant material and 5 to 45 weight percent of the fuel starvation tolerant material.
  • the catalyst comprises 30 to 70 weight % Ni or Cu, 15 to 35 weight percent of the sulfur tolerant material and 15 to 35 weight percent of the fuel starvation tolerant material.
  • some sulfur tolerant and fuel starvation tolerant materials, such as Pt may be used without Ni or Cu and comprise 100% of the catalyst.
  • the anodes may be formed using any known cermet fabrication methods.
  • the Ni or Cu metals, sulfur tolerant materials and/or the fuel starvation tolerant materials may be incorporated into the cermet by any suitable method. For example, these materials may be deposited by co-deposition, co-electrodepositon, freeze drying or sequential deposition.
  • the environmental tolerant material may be alloyed or admixed with Ni or Cu and then provided into the YSZ to form the cermet.
  • the environmental tolerant material may be alloyed or admixed with Ni or Cu and then provided into YSZ using a wet (solution), a dry (powder) or a sputtering process.
  • the environmental tolerant material may be alloyed or admixed with Ni or Cu and then placed on a support, such as a foam support or a dry ice support, and then pressed into contact with the YSZ.
  • the catalyst is diffused into the YSZ to form the cermet by sintering and/or pressing. If dry ice is used, then the dry ice is sublimed to diffuse the catalyst into the YSZ.
  • the inventor has realized that the solid oxide fuel cell system can be simplified, when feeding a hydrocarbon fuel directly to the solid oxide fuel cell anode for internal reforming to a hydrogen rich reactant by supplying the reforming process steam from the anode exhaust enthalpy recovery.
  • the product water i.e., water vapor
  • cathode enthalpy is recovered and returned to the cathode inlet to prevent the dry out of the water saturated membrane. In this case, the incoming oxidant air is humidified and membrane dry out is avoided.
  • Several methods have been developed to accomplish this water and heat transfer including hydrated membranes, water injection, and cycling desiccants.
  • One method includes using a device called an enthalpy wheel.
  • the enthalpy wheel is a porous cylindrical wheel with internal passages that are coated with desiccant. It rotates slowly in one direction, allowing the transfer of sensible and latent heat from the hot saturated air exhaust to the cool dry air inlet.
  • the present inventors realized that product water vapor emitted from the anode side exhaust of the solid oxide fuel cell may be recirculated into the fuel being provided into the anode input to prevent or reduce the carbon formation on the anode.
  • the enthalpy wheel is a preferred device to control the water and heat transferred from the anode exhaust of a solid oxide fuel cell to the anode inlet.
  • the control of the amount of water introduced with the fuel is used to prevent carbon formation with too little water and to prevent fuel starvation with too much water.
  • the water transfer rate is controlled by the speed of the wheel.
  • FIG. 27A The fundamentals of the system 600 employing an enthalpy wheel in the solid oxide fuel cell fuel stream are illustrated in FIG. 27A.
  • the hydrocarbon fuel supply is delivered through conduit 604 to enthalpy wheel 601 .
  • the fuel supply receives water vapor and heat from the anode side fuel exhaust.
  • the warm wet fuel supply is then delivered-to an optional heat exchanger 602 through conduit 605 .
  • the fuel exhaust heats the warm wet fuel supply further.
  • the hot wet fuel supply is then delivered to the anode chambers within the solid oxide fuel cell stack 603 through conduit 606 .
  • the hot wet hydrocarbon fuel supply is reformed into a mixture of hydrogen, water vapor, and carbon oxides. Nearly simultaneously, most of the hydrogen and carbon monoxide are converted to more water vapor and more carbon dioxide, respectively, from the reaction with the oxygen anions in the anode catalyst.
  • The-rotational speed of the enthalpy wheel is modulated to optimize the water vapor flux.
  • the fuel exhaust then leaves the system through outlet conduit 609 .
  • 0% to 90%, such as 20 to 70% of the product water vapor is transferred to the fuel supply.
  • all heat transferred to the fuel supply is through the enthalpy wheel and heat exchanger.
  • the enthalpy wheel is replaced with at least two adsorption beds, as illustrated in FIG. 27B.
  • the first adsorption bed 610 is used to adsorb water and water vapor from the anode exhaust, while letting anode exhaust gases, such as CO, CO 2 , H 2 and methane, to pass through to the outlet conduit 609 .
  • the second adsorption bed 611 is used to provide water that was previously collected from the anode exhaust. When the supply of water is exhausted in the second bed 611 , the anode exhaust is provided into the second bed, while the first bed 610 is used to provide the water or water vapor into the inlet fuel.
  • a reformer may also be added between the fuel inlet 604 and the fuel cell stack 603 , preferably between the heat exchanger 602 and the fuel cell stack 603 .
  • a first valve 612 such as a four way valve, switches fuel input from fuel inlet 604 between the first 610 and the second 611 adsorbent bed.
  • the valve 612 also switches the exhaust being provided from the first 610 or the second 611 beds to the outlet conduit 609 .
  • the conduit 608 connects the first adsorbent bed 610 with a first heat exchanger inlet 614 or a first heat exchanger outlet 615 via a second valve 613 , such as a four way valve.
  • the conduit 605 connects the second adsorbent bed 611 with the first heat exchanger inlet 614 or the first heat exchanger outlet 615 via valve 613 .
  • valve 613 When the valve 613 is in a first position, it provides a fluid path between the first adsorbent bed 610 and the first heat exchanger outlet 615 and between the second adsorbent bed 611 and the first heat exchanger inlet 614 .
  • valve 613 When the valve 613 is in a second position, it provides a fluid path between the first adsorbent bed 610 and the first heat exchanger inlet 614 and between the second adsorbent bed 611 and the first heat exchanger outlet 615 .
  • other configurations may be used. For example, four way valve 613 may be replaced with two three way valves, each respective valve being located between the heat exchanger 602 and respective conduits 605 , 608 .
  • the system 600 can be run without using a boiler to provide water vapor into the inlet fuel.
  • a small boiler may be added to the system. This boiler may be run during operation start up to provide water into the fuel inlet while the system is warming up and sufficient water vapor is being generated at the anode exhaust.
  • This system is advantageous because it provides simple transfer of water vapor and heat in a controlled fashion such that the proper conditions at the solid oxide fuel cell anode electrodes for internal steam reforming are met.
  • the enthalpy wheel and heat exchanger may be used to provide the entire supply of water vapor and heat for the fuel supply to operate the solid oxide fuel cell.
  • the sixth preferred embodiment is directed to a felt seal.
  • Fuel cell stacks particularly those with planar geometry, often use seals between electrolyte and interconnect surfaces to contain fuel and air (see FIG. 28). These seals must maintain their integrity at high operating temperatures and (on the cathode side) in an oxidizing environment. Furthermore, expansion and contraction of the seal and the components in contact with the seal due to thermal cycling or compression should not result in damage of any of the components during its expected life.
  • the sixth preferred embodiment is directed to a sealing arrangement that is both compliant and capable of operating at high temperatures in oxidizing and reducing environments.
  • the sealing member is capable of sealing dissimilar materials, such as a metal and a ceramic, and similar materials that may or may not differ in composition, such as two ceramics or two metals. Since the sealing member is elastic and compliant at device operating temperatures, it may be used to seal two materials with dissimilar coefficients of thermal expansion. This seal may be advantageously used in a solid oxide fuel cell, where the operating temperatures are in the range of 600 to 800° C.
  • a gas-tight compliant seal between surfaces can be made from a felt.
  • felt is used to describe a compliant layer of a material that can endure the elevated operating temperature and atmosphere of the device it is being applied to.
  • the felt may be composed of a malleable metal or alloy.
  • the compliant layer can for example be made from non-metallic fibrous materials, such as silica.
  • This compliant layer can be made up from fibers, as indicated by the word “felt,” but also other thick and compliant constructions, for example foams, such as small cell foams.
  • the seal is preferably made from a compliant metal or a ceramic fibrous or foam material.
  • the felt is made gas impermeable by one of several means, and is sealed by one of several means to the mating surfaces.
  • the felt gives compliance to the seal, allowing it to absorb stresses caused by compression and thermal expansion and contraction of the assembly of which it is part.
  • the means used to make the felt impermeable and to seal the felt to the mating surfaces are also compliant in nature. Appropriate selection of the composition of the various elements of the seal allows the seal to be made according to various criteria, including operating temperatures, oxidizing or reducing environments, and cost.
  • FIG. 28 Two mating surfaces ( 701 and 702 ) are shown in FIG. 28. A seal must be made between these two surfaces in order to prevent gas exchange in either direction between sides 705 and 706 .
  • a felt sealing member 710 is placed between the mating surfaces 701 and 702 .
  • the felt sealing member 710 is sealed to the mating surfaces through application of a sealing material 720 that is soft at the device operating temperature but is impermeable to the gases of interest in the application.
  • this may be a glass or glaze compound.
  • a glaze is a Duncan® ceramic glaze GL611. This material can be applied to the felt or to the mating surfaces prior to assembly, for example by dipping the felt sealing member and/or the mating surfaces into the molten glass or glaze. The material softens at elevated temperatures and mates the felt to the surfaces, but remains impermeable to gases.
  • the material 720 is optional if the felt seal contains appropriate means of mating the felt to the surfaces, as is the case in many preferred aspects.
  • the felt sealing member 710 is made impermeable to gases by one of several ways.
  • the porous felt is filled prior to assembly with a filler material 730 that is soft at the device operating temperature.
  • a filler material 730 that is soft at the device operating temperature.
  • this may be a glass or glaze mixture. After firing, the glassy residue makes the felt impermeable to gases, but because the material 730 softens at the operating temperature, the felt-glass composite remains compliant.
  • same-numbered items carry their previous definitions.
  • the felt sealing member 710 is made impermeable to gases by melting a felt surface 740 into a solid layer that is non-parallel, such as perpendicular, to the mating surfaces.
  • the solid layer which is formed to be thin enough to remain flexible.
  • a solid layer means a layer that has a much lower porosity than the felt, such as a porosity of 70% or less than the felt.
  • This solid layer may be formed by selectively heating a portion of the felt sealing member 710 to transform the heated portion to a solid layer, such as a closed cell metal foam layer.
  • a surface 740 of the felt sealing member 710 may be selectively heated by a laser to form the solid layer.
  • the felt sealing member 710 is made impermeable to gases by forming a solid layer 750 on felt sealing member 710 that is perpendicular and parallel to the mating surfaces described previously.
  • the parallel solid surfaces provide an improved contact area for the seal.
  • the felt sealing member 710 is made impermeable to gases through application of a barrier foil layer 760 that is non-parallel, such as perpendicular, to the mating surfaces.
  • the foil adheres to the felt via a material such as that which is used to attach the felt to the mating surfaces.
  • the foil may be pressed into place and held by a second felt sealing member or other component.
  • the foil 760 is compliant because it is thin.
  • the foil is a thin metal foil.
  • the foil extends between mating surfaces 701 , 702 to block the flow of gas between sides 705 and 706 .
  • the felt sealing member 710 is made impermeable to gases through application of several foils.
  • Foil 770 is non-parallel, such as perpendicular, to the mating surfaces as described previously, and foils 772 and 774 extend into the area parallel to the mating surfaces. These foils 772 , 774 provide improved contact area for the sealing member. They may also produce adhesion between the sealing member and the mating surfaces.
  • the foils 770 , 772 , and 774 may be the same or different materials depending on the various compositions of the felt 710 and mating surfaces 701 and 702 . They may comprise separate components or one continuous piece of foil.
  • the felt sealing member 710 is made impermeable to gases through deposition of a gas impermeable material layer on the felt 710 .
  • This material may be deposited on the felt by various methods, including but not restricted to, dipping and evaporation, physical vapor deposition, chemical vapor deposition, thermal spray, plasma spray, and precipitation from a liquid.
  • Material portion 780 is non-parallel, such as perpendicular, to the mating surfaces 701 , 702 .
  • portions 782 , 784 of the gas impermeable material layer extend into the area parallel to the mating surfaces 701 , 702 . These portions 782 , 784 provide an improved contact area for the sealing member.
  • the impermeable material layer portions 780 , 782 , and 784 may be the same or different materials depending on the various compositions of the felt 710 and mating surfaces 701 and 702 .
  • the felt sealing member 790 is made impermeable to gases in its initial preparation.
  • the felt may be prepared as a closed-cell foam.
  • the felt composition can be selected so as to operate well in the atmosphere present in the device containing the felt seal.
  • the felt in an oxidizing atmosphere the felt may be composed of a suitable M—Cr—Al—Y material, where M comprises at least one metal selected from Fe, Co, or Ni.
  • the felt in another example, the felt may be composed of Inconel alloy.
  • the felt in a reducing atmosphere, the felt may be composed of nickel.
  • Other metals, alloys, or indeed other malleable materials or compounds metal may be used depending on the application requirements.
  • One example of forming a felt sealing member 710 (nickel felt) with a gas impermeable material 730 (glass) is as follows.
  • a nickel felt i.e.
  • foam with a density of 15% relative to solid nickel is saturated with a molten glass.
  • the felt is fired to remove volatiles, leaving behind a glass residue that renders the felt impermeable to gases.
  • the felt is placed between two mating surfaces, for example a metal sheet and zirconia. To each of the mating surfaces a layer of glass seal is applied where the felt-glass composite will contact the surfaces. The felt is placed between the surfaces, compressed, and fired.
  • the seal can take the shape of the mating surfaces to be sealed.
  • the seal may take the form of a rectangular gasket.
  • the mating surfaces contain open areas, such as in an assembly with internal gas manifolds or flow ducts, the seal can accommodate and seal such open areas. This is illustrated in FIG. 35, where one of the mating surfaces ( 794 ) contains flow channels which are sealed from the center of the surface and from the exterior of the surface by the felt gasket 797 .
  • All embodiments of the felt seal can be placed in a structure in one or both mating surfaces, for example in a groove in a mating surface, that provides containment and additional compression and adhesion surfaces.
  • the felt part of the seal may also serve other roles, such as current collector/distributor, flow distributor, etc. in a fuel cell stack, such as a solid oxide fuel stack.
  • the seventh preferred embodiment is directed to felt current conductors/gas flow distributors for fuel cell stacks.
  • Fuel cell stacks particularly those with planar geometry, often use utilize some material to conduct electrons from the anode to the separator plate and from the separator plate to the cathode.
  • This material typically has a better electrical conductivity than the porous electrode (i.e., anode and/or cathode) material.
  • this material is distinguished from the electrodes in that it also must provide flow distribution of oxygen- or fuel-bearing gases.
  • This material is often called a current conductor/gas flow distributor (“conductor/distributor” herein after).
  • these conductor/distributors may provide structural support to the fuel cell stack.
  • Some examples of prior art conductor/distributors include metal wire coils, wire grids, and metal ribs. These may be used independently or in some combination.
  • the prior art conductor/distributors sometimes exhibit less-than-optimal current conduction or gas flow distribution properties. They are also costly to implement. Also, many of the prior art conductor/distributors are not compliant (i.e., not elastic at the fuel cell operating temperatures). Non-compliant components often present difficulties and high costs in fabrication and assembly of the fuel cells due to the tighter fuel cell tolerances which are required.
  • a porous conductive felt can serve as a current conductor and gas flow distributor with better properties than the prior art conductor/distributors and may be less costly to implement.
  • the felt conductor/distributor can also serve as a seal or as a support for other fuel cell stack components.
  • the use of a compliant, conductive felt reduces the probability of component and assembly failure during thermal cycling and compression of a fuel cell stack, preferably a high temperature fuel cell stack, such as a solid oxide or molten carbonate fuel cell stack.
  • conductive felt is used to describe a compliant layer of electrically conductive material that can endure the operating temperature and atmosphere of the device (i.e., fuel cell stack) in which it is located.
  • the felt may be composed of a malleable metal or alloy.
  • this definition does not restrict the term “felt” to metals.
  • the felt conductor/distributor can for example be made from other porous, conductive materials, such as a silica-metal composite.
  • the felt conductor/distributor should be made conductive and gas permeable and can be made up from fibers, foams and other relatively thick, compliant, conductive and gas permeable structures.
  • a conductor/distributor comprising a gas permeable (i.e., porous) conductive felt with composition chosen to be appropriate for the conditions specified by the application.
  • the felt material is chosen such that it remains conductive and gas permeable at the fuel cell operating temperature.
  • the felt conductor/distributor is located in contact with the active area of the fuel electrode (i.e., anode or cathode).
  • the fuel cell separator plate is placed in contact with the conductor/distributor.
  • Various ways may be used to ensure electrical contact between electrode, conductor/distributor, and separator plate.
  • FIG. 36 shows repeating elements of a fuel cell stack containing an electrolyte 810 , an anode 820 , a cathode 830 , anode seal 840 , cathode seal 845 , and a separator plate 850 , such as metal plates.
  • a second separator plate 850 is also shown in the diagram to illustrate the connection to the next cell of the stack.
  • the stack may be internally or externally manifolded, as will be described in more detail below.
  • the anode 820 and cathode 830 are often optimized for the electrochemical reactions they are catalyzing. Often, they are not optimized for electrical conductivity or for distribution of fuel- and oxygen-bearing gases. Therefore, anode conductor/distributors 860 and cathode conductor/distributors 870 are provided to fill these roles.
  • the separator plates 850 may be omitted if the felt conductor/distributors are constructed to also perform the function of the separator plates.
  • the anode conductor/distributor 860 is composed of a conductive felt.
  • the felt conducts electrons from the anode to the separator plate. Since the felt is gas permeable, it also allows fuel to reach the anode surface, and the reaction byproducts to leave the surface and exhaust from the cell.
  • the electrical contact between anode and felt, and between separator plate and felt, may be enhanced by adding a layer of an optional adhesive or contact material.
  • the composition of the felt is chosen as appropriate for the fuel cell operating conditions.
  • a nickel felt with a density of 15 to 35%, preferably about 25% relative to the density of solid nickel and a thickness of 0.5 to 4 mm, preferably about 2 mm may be used in a high temperature fuel cell, such as a solid oxide fuel cell, with a reducing atmosphere and a temperature of 600 to 850° C., such as 800° C.
  • the felt may be potted in a nickel-YSZ cermet on either the anode or separator plate sides of the connection, or on both sides.
  • the cathode conductor/distributor 870 is composed of a conductive felt.
  • the felt conducts electrons from the separator plate to the cathode. It also allows oxygen to reach the cathode surface, and the oxygen depleted air to leave the surface and exhaust from the cell.
  • the electrical contact between cathode and felt, and between separator plate and felt, may be enhanced by adding a layer of an optional adhesive or contact material.
  • the composition of the felt is chosen as appropriate for the fuel cell operating conditions.
  • a Fe—Cr—Al—Y felt with a density of 5 to 30%, preferably about 15% relative to the density of the solid metal alloy and a thickness of 0.5 to 4 mm, preferably 2 mm, may be used in a high temperature fuel cell, such as a solid oxide fuel cell, in an oxidizing atmosphere at 650 to 850° C., such as about 800° C.
  • a high temperature fuel cell such as a solid oxide fuel cell
  • an oxidizing atmosphere at 650 to 850° C., such as about 800° C.
  • some or all of Fe may be substituted by Co and/or Ni in the Fe—Cr—Al—Y felt.
  • the felt may be potted in a lanthanum-strontium manganite (LSM) perovskite on either the cathode or separator plate sides of the connection, or on both sides.
  • LSM lanthanum-strontium manganite
  • both the anode 860 and cathode 870 conductor/distributors are made from a felt.
  • same-numbered items carry their previous definitions.
  • the anode and/or cathode conductor/distributors contain a non-uniform surface.
  • the conductor/distributor(s) contain ribs which provide a desired pressure drop or flow distribution pattern.
  • Other surface features, such as dimples, lines, or a particular pore geometry may be used to exercise control over pressure drop or flow distribution.
  • the anode conductor/distributor 860 is combined with the anode-side felt seal of the sixth preferred embodiment.
  • the anode conductor/distributor and seal is made of one continuous piece of material.
  • the anode conductor/distributor 860 can be used in conjunction with any of the various preferred aspects of the sixth embodiment describing the felt seal.
  • the cathode conductor/distributor 870 is combined with the cathode-side felt seal of the sixth preferred embodiment.
  • the cathode conductor/distributor and seal is made of one continuous piece of material.
  • the cathode conductor/distributor 870 can be used in conjunction with any of the various preferred aspects of the sixth embodiment describing the felt seal. Most preferably, both the anode and cathode conductor/distributors are combined with the felt seal.
  • the anode conductor/distributor 860 provides the structural support for the separator plate 850 .
  • the separator plate material may be made as thin as practicality and serviceability allows.
  • the separator plate comprises a thin film deposited onto the anode conductor/distributor 860 by various thin film deposition techniques, including but not limited to thermal or plasma spray, chemical or physical vapor deposition (i.e., CVD or sputtering), precipitation, and dipping.
  • the thin separator plate 850 may comprise an integral component that is placed in contact with the conductor/distributor.
  • a “thin film” is less than 500 microns thick, more preferably, less than 100 microns thick, most preferably 10 to 30 microns thick.
  • the felt conductor/distributor thickness is sufficient to act as a substrate for the thin film, such as a thickness of greater than 30 microns, preferably greater than 100 microns.
  • the cathode conductor/distributor 870 provides the structural support for the separator plate 850 .
  • the separator plate material may be made as thin as practicality and serviceability allows.
  • the separator plate comprises a thin film deposited onto the cathode conductor/distributor 870 by various thin film deposition techniques, including but not limited to thermal or plasma spray, chemical or physical vapor deposition (i.e., CVD or sputtering), precipitation, and dipping.
  • the thin separator plate 850 may comprise an integral component that is placed in contact with the conductor/distributor.
  • both the anode and cathode conductor/distributors serve as a support for their respective separator plates.
  • the anode conductor/distributor 860 serves as a seal and as separator plate support.
  • the anode conductor/distributor renumbered 865 is shown in one of its various preferred configurations.
  • the cathode conductor/distributor 870 serves also as seal and as separator plate support.
  • the cathode conductor/distributor renumbered 875 is shown in one of its various preferred configurations.
  • the anode conductor/distributor 865 and the cathode conductor/distributor 875 together support a common separator plate 850 that is located between them.
  • the separator plate 850 may be placed or deposited in any way so as to reduce the materials and assembly costs and increase the performance and quality of the assembly.
  • the separator plate 850 would be made as thin as practicality and serviceability allows, such as a thin film plate.
  • the seal portions of the conductor/distributors can be made gas impermeable by any of the methods described in the sixth preferred embodiment.
  • portions of the separator plate 850 may be used to form a seal.
  • thin separator plate material or foil can be extended around the edges of either or both conductor/distributors as shown in FIG. 44. These separator plate extension act as a gas impermeable seal.
  • the anode conductor/distributor 865 and the cathode conductor/distributor 875 together support not only the separator plate 850 , but they also support the cathode 830 , electrolyte. 810 , and anode 820 .
  • the separator plate 850 , cathode 830 , electrolyte 810 , and anode 820 may be placed or deposited in any way so as to reduce the materials and assembly costs and increase the performance and quality of the assembly.
  • these components would be made as thin as practicality and serviceability allows.
  • These components preferably comprise thin films (as defined above) that are preferably deposited on the conductor/distributor 865 / 875 “substrate” by various thin film deposition techniques described above.
  • FIG. 46 illustrates a three dimensional view of an internally manifolded fuel cell stack containing a common felt conductor/distributor and seal.
  • the fuel cell stack contains a separator plate 850 , an anode felt conductor/distributor/seal 860 , an electrolyte 810 , and anode 820 and a cathode felt conductor/distributor/seal 870 .
  • the cathode is not visible in FIG. 46 because it is located “behind” the electrolyte 820 .
  • the separator plate 850 and electrolyte 810 contain gas passages or openings 876 , 877 , 878 and 879 . Specifically, passages 876 are fuel inlet passages, passages 877 are fuel outlet passages, passages 878 are oxidizer inlet passages and passages 879 are oxidizer outlet passages.
  • the anode felt conductor/distributor/seal 860 is made of a conductive felt.
  • the entire anode felt conductor/distributor/seal 860 is gas permeable, except for gas impermeable seal region or strip 880 .
  • the cathode felt conductor/distributor/seal 870 is made of a conductive felt.
  • the entire cathode felt conductor/distributor/seal 870 is gas permeable, except for gas impermeable seal region or strip 881 .
  • the gas impermeable strip 880 circumscribes a gas permeable region 882 and seals it from a gas permeable region 883 .
  • the gas impermeable strip 881 circumscribes a gas permeable region 884 and seals it from a gas permeable region 885 .
  • Region 882 lines up with the anode 820 and with the fuel passages 876 and 877 when the stack is assembled.
  • Region 883 lines up with the oxidizer passages 878 and 879 .
  • Region 884 lines up with the cathode (not shown) and with the oxidizer passages 878 and 879 .
  • Region 885 lines up with fuel passages 876 and 877 .
  • the fuel cell stack operates as follows.
  • the input or inlet fuel 886 (dashed lines in FIG. 46) is provided into fuel inlet passage 876 in separator plate 850 .
  • the fuel reaches the gas permeable region 882 in the anode conductor/distributor/seal 860 . From here, the input fuel splits into two directions. One part of the fuel travels “down” through gas permeable felt region 882 and reacts at the anode 820 .
  • the fuel reaction products 887 then exit from region 882 through fuel outlet passage 877 in the separator plate 850 .
  • Another part of the fuel travels through passage 876 in the electrolyte and passes through the gas permeable region 885 in the cathode conductor/distributor/seal 870 .
  • the gas impermeable strip or seal 880 prevents the fuel from entering region 883 and reacting with the oxidizer.
  • the gas impermeable strip or seal 881 prevents the fuel from entering region 884 and contacting the cathode.
  • the input or inlet oxidizer 888 (dotted-dashed lines in FIG. 46) is provided into oxidizer inlet passage 878 in separator plate 850 .
  • the oxidizer passes through the gas permeable region 883 in the anode conductor/distributor/seal 860 .
  • the oxidizer then travels through passage 878 in the electrolyte and reaches the gas permeable region 884 in the cathode conductor/distributor/seal 870 . From here, the input oxidizer splits into two directions. One part of the oxidizer travels “right” through gas permeable felt region 884 and reacts at the cathode.
  • the reacted oxidizer 889 then travels back and exits from region 884 through oxidizer outlet passage 879 in the separator plate 850 .
  • the gas impermeable strip or seal 880 prevents the oxidizer from entering region 882 and contacting the anode.
  • the gas impermeable strip or seal 881 prevents the oxidizer from entering region 885 and reacting with the fuel.
  • the gas impermeable regions 880 , 881 may be formed by any method described in the sixth embodiment, such as by selective heating or laser irradiation or selective addition of a gas impermeable material to the felt.
  • the gas impermeable regions 880 , 881 act as felt seals in the felt conductor/distributors 860 , 870 . They separate and prevent the fuel and oxidizer from contacting each other in the fuel cell stack.
  • the fuel stacks and the seals 880 , 881 may have any suitable shape and should not be considered limited to the shape illustrated in FIG. 46.
  • “down” and “right” are relative directions depending on the orientation of the fuel cell stack. It should be noted that the fuel and oxidizer cross the fuel stack in different, preferably perpendicular directions.
  • the felt conductor/distributor/seals are not limited to unitary conductive felt sheets 860 , 870 containing both the gas impermeable seals 880 , 881 and the gas permeable conductor/distributors 882 , 884 .
  • the gas impermeable seals may be formed in separate felt gaskets that are placed adjacent to the gas permeable felt conductor/distributors, as shown in FIG. 47.
  • the conductive felt anode conductor/distributor/seal 890 comprises a gas impermeable felt gasket 891 and a gas permeable felt conductor/distributor 860 .
  • the gasket 891 contains a large opening 892 , which lines up with the conductor/distributor 860 and with the fuel inlet and outlet passages 876 , 877 in the separator plate 850 and the electrolyte 810 (shown in FIG. 46).
  • the inlet fuel enters the conductor/distributor through opening 892 and travels to the anode 820 .
  • the one large opening 892 may be replaced with two smaller openings which line up with the conductor/distributor and the fuel passages 876 , 877 in the separator plate 850 and electrolyte 810 .
  • the gasket 891 also contains the oxidizer inlet and outlet passages 878 A, 879 A, which do not line up with the anode conductor/distributor 860 . Thus, the oxidizer travelling through these passages does not enter the conductor/distributor 860 and does not reach the anode.
  • the conductive felt cathode conductor/distributor/seal 895 comprises a gas impermeable felt gasket 896 and a gas permeable felt conductor/distributor 870 .
  • the gasket 896 contains a large opening 897 , which lines up with the conductor/distributor 870 and with the oxidizer inlet and outlet passages 878 , 879 in the separator plate 850 and the electrolyte 810 (shown in FIG. 46).
  • the inlet oxidizer enters the conductor/distributor through opening 897 and travels to the cathode 830 .
  • the one large opening 897 may be replaced with two smaller openings which line up with the conductor/distributor and the oxidizer passages 878 , 879 in the separator plate 850 and electrolyte 810 .
  • the gasket 896 also contains the fuel inlet and outlet passages 876 A, 877 A, which do not line up with the cathode conductor/distributor 870 . Thus, the fuel travelling through these passages does not enter the conductor/distributor 870 and does not reach the cathode.
  • the conductor/distributor/seals may also be used in externally manifolded fuel cells, as shown in FIG. 48.
  • the alternating conductive felt anode and cathode conductor/distributor/seals 860 , 870 are shown as being located in a fuel cell stack housing 899 .
  • the housing may have a cylindrical or any other suitable shape.
  • the thin electrolyte, separator plates and electrodes are located between the conductor/distributor/seals 860 , 870 , but are not shown in FIG. 48 for clarity.
  • passage 876 B is a fuel inlet passage
  • passage 877 B is a fuel outlet passage
  • passage 878 B is an oxidizer inlet passage
  • passage 879 B is an oxidizer outlet passage.
  • the “vertical” (i.e., “left” and “right”) surfaces 880 A of anode conductor/distributor/seals 860 are rendered gas impermeable.
  • the “horizontal” (i.e., “top” and “bottom”) surfaces 881 A of cathode conductor/distributor/seals 870 are also rendered gas impermeable.
  • the remainder of the conductor/distributor/seals 860 , 870 remains gas permeable.
  • the sealing may be accomplished by any method described in the sixth embodiment, such as by selective heating or laser irradiation, selective impregnation of the surfaces with a gas impermeable material (i.e., such as by dipping into such material), by selective deposition of foils or thin films on the desired surfaces, or by bending portions of the separator plates around the desired surface edges.
  • the fuel from passage 876 B travels through gas permeable surfaces 882 A of sheets 860 to reach the anode.
  • the oxidizer from passage 878 B travels through gas permeable surfaces 884 A of sheets 870 to reach the cathode.
  • the fuel in passages 876 B and 877 B does not permeate through surfaces 881 A, and does not react with the oxidizer or reach the cathode.
  • the oxidizer in passages 878 B and 879 B does not permeate through surfaces 880 , A and does not react with the fuel or reach the anode.
  • the fuel stacks and the conductor/distributors 860 , 870 may have any suitable shape and should not be considered limited to the shape illustrated in FIG. 48. Furthermore, “vertical” and “horizontal” are relative directions depending on the orientation of the fuel cell stack. It should be noted that the fuel and oxidizer cross the fuel stack in different, preferably perpendicular directions.
  • the various components of the systems and fuel cells and steps of the methods described in the first through the seventh embodiments may be used together in any combination.
  • the components and systems of all seven embodiments are used together.
  • the preferred method and system include a temperature sensitive adsorption oxygen enrichment method and system of the first embodiment, a load matched power generation system including a solid oxide fuel cell and a heat pump and an optional turbine, and method of using the system of the second embodiment, a textured fuel cell ceramic electrolyte of the third embodiment, an environment tolerant fuel cell anode catalyst of the fourth embodiment, a water vapor replenishment system including the preferred enthalpy wheel of the fifth embodiment, a felt seal in the fuel cell of the sixth embodiment and a felt collector of the seventh embodiment.
  • any one, two, three, four or five of the above features may be omitted from the preferred system, fuel cell and method.

Abstract

A system contains a solid oxide fuel cell stack and an enthalpy wheel or at least two adsorbent beds. The enthalpy wheel or the adsorbent beds transfer product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply.

Description

  • This application claims benefit of priority of U.S. provisional application No. 60/357,636 filed on Feb. 20, 2002, which is incorporated by reference in its entirety. The present invention is directed generally to fuel cells and more particularly to solid oxide fuel cells and power generation systems.[0001]
  • FIELD OF THE INVENTION BACKGROUND OF THE INVENTION
  • Fuel cells generate electricity from hydrogen or various hydrocarbon fuels. In some fuel cells, an oxygen containing gas, such as air, is provided onto the cathode side of the electrolyte, while hydrogen or a hydrocarbon fuel is provided onto the anode side of the electrolyte. The fuel cell generates electricity through an electrochemical reaction. For example, in a solid oxide fuel cell, oxygen containing air is provided onto the cathode side of a solid ceramic electrolyte, while a hydrocarbon fuel is provided onto the anode side of the electrolyte. [0002]
  • Fuel cells operate more efficiently when the oxygen content of the inlet air is higher, primarily because the Nernst potential of the cell increases when the partial pressure of oxygen is higher. Therefore, the oxygen content of air being provided into the fuel cell is sometimes increased or enriched using various processes, including pressure swing adsorption (e.g., QuestAir Inc.'s Pulsar technology), oxygen-selective membranes (e.g., Boyer et al., J. Appl. Electrochem., p.1095, 1999), or magnetic separation devices (e.g., Nitta et al., U.S. Pat. No. 6,106,963, incorporated herein by reference in the entirety). However, these methods are generally inefficient because they require the use of power (i.e., electricity), thus decreasing the efficiency of the fuel cell and the power generation system. [0003]
  • BRIEF SUMMARY OF THE INVENTION
  • One preferred embodiment of the present invention provides a system, comprising a solid oxide fuel cell stack, and an enthalpy wheel which transfers product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply. [0004]
  • Another preferred embodiment of the present invention provides a system comprising a solid oxide fuel cell stack, at least two adsorbent beds which transfer product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply. [0005]
  • Another preferred embodiment of the present invention provides a system comprising a solid oxide fuel cell stack, and a first means for transferring product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply. [0006]
  • Another preferred embodiment of the present invention provides a method of hydrating fuel provided into a solid oxide fuel cell stack, comprising providing a hydrocarbon fuel into an anode input of solid oxide fuel cell stack, and transferring product water vapor from a fuel cell stack anode exhaust into a fuel cell stack fuel supply.[0007]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIGS. [0008] 1-5 are schematic representations of oxygen enrichment systems according to the first preferred embodiment.
  • FIGS. [0009] 6-10D are schematic representations of a combined electrical power generation and cooling system according to the second preferred embodiment.
  • FIG. 11 is a schematic side cross sectional view of a prior art solid oxide fuel cell. [0010]
  • FIG. 12 is a schematic illustration of oxygen transport through the electrolyte. [0011]
  • FIGS. 13, 15 and [0012] 16 are schematic side cross sectional views of solid oxide fuel cells according to the third preferred embodiment.
  • FIG. 14 is a schematic side cross sectional view of a prior art multi-layer solid oxide electrolyte. [0013]
  • FIGS. [0014] 17-24 are schematic side cross sectional views of methods of making the electrolyte according to the third preferred embodiment.
  • FIGS. [0015] 25-26 are schematic side cross sectional views of fuel cells according to the fourth preferred embodiment.
  • FIGS. 27A and 27B are schematic diagrams of systems according to the fifth preferred embodiment. [0016]
  • FIGS. [0017] 28-35 are schematic representations of seals according to the sixth preferred embodiment.
  • FIGS. [0018] 36-48 are schematic representations of the repeating elements of a fuel cell stack, including the felt current conductor/flow distributor elements, according to the seventh preferred embodiment.
  • FIGS. [0019] 36-45 are cross-sectional, exploded views and FIGS. 46-48 are three dimensional cut away views.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • I. The First Preferred Embodiment [0020]
  • In a first preferred embodiment of the present invention, the inventors have realized that the oxygen content of air being provided into the fuel cell can be increased using a temperature sensitive adsorption cycle. Preferably, the temperature sensitive adsorption cycle utilizes the heat generated by the fuel cell during power generation. The use of heat generated by a fuel cell for increasing the oxygen content of the inlet air stream in a cyclical adsorption separation process increases the efficiency of power generation. However, heat generated by means other than the fuel cell may be used instead. [0021]
  • In the temperature sensitive adsorption process, an air stream (a mixture of nitrogen and oxygen) is passed through a cool adsorbent medium that selectively removes a fraction of the nitrogen, resulting in a gas stream that has a higher oxygen content than the original stream. When the adsorbent is saturated with nitrogen under the process conditions, heat generated from the fuel cell operation or from another source is transferred to the adsorbent medium, and the nitrogen is driven out of the adsorbent medium through a vent. Thus, a separation is effected. [0022]
  • FIG. 1 schematically illustrates the temperature sensitive [0023] oxygen enrichment system 1. The system includes an air source 3, an adsorbent medium 5 and a fuel cell 7. The air source 3 may be an air blower, an air inlet conduit and/or any other device which provides air into the adsorbent medium 5. The adsorbent medium 5 may be any medium which selectively adsorbs nitrogen compared to oxygen. Preferably, the adsorbent medium 5 is a bed containing a nitrogen adsorbing material, such as a zeolite or a mixture of zeolites. For example, silver X, sodium X or calcium A zeolites may be used. The fuel cell 7 may be any fuel cell into which air is provided. Preferably, the fuel cell 7 is a solid oxide fuel cell. However, other fuel cells, such as PEM, direct methanol, molten carbonate, phosphoric acid or alkaline fuel cells may be used.
  • The [0024] system 1 also preferably contains a heat transfer conduit 9 located between the fuel cell 7 and the adsorbent medium 5. The conduit 9 transfers heat from the fuel cell 7 to the adsorbent medium 5. The conduit 9 may comprise any device than may transfer heat from one location to another. For example, the conduit 9 may comprise a pipe, a duct, a space between walls or even a solid heat transfer material. Preferably the conduit 9 is a pipe which transfers a heat transfer fluid through the system 1.
  • An [0025] air inlet 11 is located in the adsorbent medium 5 housing. The inlet provides air from the air source 3 into the adsorbent medium 5. An oxygen enriched air conduit 13 is located between the adsorbent medium 5 and the fuel cell 7. The conduit 13 may be pipe, duct or open space which provides oxygen enriched air from the adsorbent medium 5 to the fuel cell 7.
  • In one preferred aspect of the first embodiment, the heat transfer conduit [0026] 9 comprises a pipe which is located adjacent to the fuel cell 7, adjacent to a heat sink 15 and adjacent to the adsorbent medium 5. For example, as shown in FIG. 2, the conduit 9 is wrapped around the housing of the adsorbent medium 5 and around the fuel cell 7. The conduit 9 also passes through the heat sink 15. The heat transfer conduit 9 transfers a heated heat transfer liquid, such as water, from adjacent to the fuel cell 7 to the adsorbent medium 5. The heated heat transfer liquid heats the adsorbent medium 5 to desorb nitrogen from the adsorbent medium 5. The heat transfer conduit 9 also transfers a cooled heat transfer liquid, such as water, from adjacent to the heat sink 15 to the adsorbent medium 5. The cooled heat transfer liquid cools the adsorbent medium 5, which allows the adsorbent medium 5 to adsorb nitrogen from air that is being provided from inlet 11.
  • The operation of the heat transfer conduit [0027] 9 illustrated in FIG. 2 will now be described in more detail. The conduit 9 is filled with a heat transfer liquid. This liquid may be any liquid which is capable of transferring heat. Preferably, this liquid is water. However, other liquids, such as mineral oil, etc., or even heat transfer gases may be used. The liquid is provided through conduit 9 and through at least one valve. Preferably, the conduit 9 contains an outlet valve 17 and an inlet valve 19. However, only one of these two valves may be used. The outlet valve 17 is preferably a three way valve which directs the liquid either through a first segment 21 of the conduit 9, through a second segment 23 of the conduit 9, or prevents liquid flow through the conduit 9. If liquid is provided through the first segment 21 which is located adjacent to the fuel cell 7, then the liquid is heated by the heat generated in the fuel cell 7. For example, “located adjacent” means that the first segment 21 of the conduit 9 is wrapped around the fuel cell 7 or a stack of fuel cells if more than one fuel cell is used. However, “located adjacent” also includes any other configuration of segment 21 which allows the fuel cell 7 to heat the liquid in the segment 21. For example, the segment 21 may be located in contact with one or more surfaces of the fuel cell 7 or segment 21 may be located near the fuel cell, rather than being wrapped around the fuel cell.
  • The heated heat transfer liquid is then provided from the [0028] first segment 21 through the inlet valve 19 into the portion of conduit 9 that is located adjacent to the adsorbent medium 5. For example, “located adjacent” means that the conduit 9 is wrapped around the housing of the adsorbent medium 5. However, “located adjacent” also includes any other configuration of conduit 9 which allows the heat transfer liquid to heat the adsorbent medium 5. For example, the conduit 9 may be located in contact with one or more surfaces of the adsorbent medium 5 or conduit 9 may be located near the adsorbent medium 5, rather than being wrapped around it. The heated heat transfer liquid heats the adsorbent medium 5 and desorbs the nitrogen adsorbed in the adsorbent medium 5.
  • When it is desired to cool the [0029] adsorbent medium 5, then the valves 17 and 19 are switched to provide the heat transfer fluid through a second segment 23 of the conduit 9. The second segment 23 is located adjacent to a heat sink 15. The heat sink 15 may comprise any thing which can cool the liquid in the second segment 23 of the conduit 9. For example, the heat sink 15 may be a cooling tower, a heat exchanger, a radiator with cool air, a cold air blower or even a portion of segment 23 which runs through the cool ground or wall. The segment 23 may pass through the heat sink 15 or be placed in contact with or adjacent to the heat sink 15, depending on what type of heat sink is used.
  • The cooled heat transfer liquid is then provided from the [0030] second segment 23 through the inlet valve 19 into the portion of conduit 9 that is located adjacent to the adsorbent medium 5. The cooled heat transfer fluid cools the adsorbent medium 5 while air from inlet 11 is passing through the adsorbent medium 5 to desorb nitrogen from the air.
  • As shown in FIG. 2, the heat transfer liquid is provided through the conduit [0031] 9 in a closed control loop. The system 1 of FIG. 2 operates in a batch or non-continuous mode. Thus, when air is provided from the air source 3 through the adsorbent medium 5 into the fuel cell 7, the heat transfer liquid is passed through the second segment 23 adjacent to the heat sink 15. The cooled heat transfer liquid cools the adsorbent medium 5 to adsorb the nitrogen from the air. When no air is provided from the air source 3 through the adsorbent medium 5 into the fuel cell 7, the heat transfer liquid is passed through the first segment 21 adjacent to the fuel cell 7. The heated heat transfer liquid heats the adsorbent medium 5 to desorb the nitrogen.
  • However, in a second preferred aspect of the first embodiment, the [0032] system 1 operates in a continuous mode. To operate in a continuous mode, the system 100 contains two or more adsorbent mediums 5A, 5B, as shown in FIG. 3. In FIG. 3, elements with like numbers to elements in FIGS. 1-2 are presumed to be the same. In the preferred aspect of FIG. 3, while one adsorbent medium 5A is used to adsorb nitrogen to oxygen enrich the air being provided into the fuel cell, the other adsorbent medium 5B is heated by the heat from the fuel cell to desorb the nitrogen from the adsorbent medium 5B.
  • The [0033] system 100 shown in FIG. 3 contains the following elements. The system 100 contains one or more air sources 3, such as blowers, and a plurality of adsorbent mediums 5A, 5B which selectively adsorb nitrogen compared to oxygen. While only two mediums are shown in FIG. 3, there may be more than two mediums if desired. The system 100 also contains a plurality of heat transfer conduits 9A, 9B which transfer heat from the fuel cell (not shown in FIG. 3 for clarity) to the plurality of adsorbent mediums 5A, 5B. The conduits 9A, 9B are located between the fuel cell and the plurality of adsorbent mediums 5A, 5B.
  • There are also a plurality of [0034] air inlets 11A, 11B into the plurality of adsorbent mediums 5A, 5B, and a plurality of outlets 13A, 13B (i.e., a plurality of oxygen enriched air conduits) which provide oxygen enriched air from the plurality of adsorbent mediums 5A, 5B to the fuel cell. The conduits 13A, 13B are located between the plurality of adsorbent mediums 5A, 5B and the fuel cell.
  • Preferably, the [0035] system 100 contains seven three way valves, as will be described in more detail below. However, more or less than seven valves may be used as desired. The system 100 contains least one inlet selector valve 27 located between the air source 3 and the plurality of adsorbent mediums 5A, 5B. The inlet selector valve 27 directs air from the air source 3 into either a first adsorbent medium 5A or into a second adsorbent medium 5B.
  • The [0036] system 100 also contains at least one outlet selector valve 29 located between the plurality of adsorbent mediums 5A, 5B and the fuel cell. The outlet selector valve 29 directs oxygen enriched air into the fuel cell through oxygen enriched air conduits 13A, 13B, 13C from either the first adsorbent medium 5A or from the second adsorbent medium 5B.
  • The [0037] system 100 contains at least one venting selector valve 31 located between the air source 3 and the plurality of adsorbent mediums 5A, 5B. The venting selector valve 31 directs desorbed nitrogen to be vented through vent 25 from either the second adsorbent medium 5B or from the first adsorbent medium 5A.
  • At least one connecting [0038] conduit 33 is provided such that it connects a plurality of oxygen enriched air conduits 13A, 13B. The connecting conduit 33 directs purging air from one of the first or the second adsorbent medium to the other one of the first or the second adsorbent medium to purge the nitrogen from the receiving medium. Preferably, the conduit 33 contains one or more flow restrictors 35. The restrictors 35 restrict the flow of oxygen enriched air, such that the majority of the oxygen enriched air exiting an adsorbent medium is directed to the fuel cell through conduit 13C, rather than through the connecting conduit 33.
  • The [0039] system 100 contains at least one heat transfer fluid inlet valve 37A, 37B located in the heat transfer fluid conduits 9A, 9B. Preferably there are two such valves as shown in FIG. 3. Valve 37A directs heated heat transfer fluid to the one of the adsorbent mediums 5A, 5B from the fuel cell stack, while valve 37B directs cooled heat transfer fluid to another one of the adsorbent mediums 5A, 5B from the heat sink.
  • Furthermore, the [0040] system 100 contains at least one heat transfer fluid outlet valve 39A, 39B located in the heat transfer fluid conduits 9A, 9B. Preferably there are two such valves as shown in FIG. 3. Valve 39A directs heated heat transfer fluid from the adsorbent mediums to the heat sink, while valve 39B directs cooled heat transfer fluid from the adsorbent mediums to the fuel cell.
  • Thus, the [0041] conduits 9A, 9B actually comprise two segments of one common conduit 9. For example, the output of conduit 9A is provided through valve 39B, the fuel cell stack and valve 37A to input of conduit 9B, while the output of conduit 9B is provided through valve 39A, the heat sink and valve 37B to input of conduit 9A. However, the valves 37A, 37B and 39A, 39B may be set such that the conduits 9A and 9B remain separate, as will be discussed in more detail below.
  • The method of [0042] operating system 100 will now be described with respect to FIGS. 3 and 4. As shown in FIG. 3, the valves are set to allow the first adsorbent medium 5A to provide oxygen enriched air into the fuel cell, while the nitrogen is desorbed from the second adsorbent medium 5B. The first adsorbent medium 5A is cooled by a cool heat transfer fluid in conduit 9A, while the second adsorbent medium 5B is heated by a hot heat transfer fluid in conduit 9B.
  • Then, after some time, the valve positions are switched as shown in FIG. 4. As shown in FIG. 4, the valves are set to allow the second adsorbent medium [0043] 5B to provide oxygen enriched air into the fuel cell, while the nitrogen is desorbed from the first adsorbent medium 5A. The second adsorbent medium 5B is cooled by a cool heat transfer fluid in conduit 9B, while the first adsorbent medium 5A is heated by a hot heat transfer fluid in conduit 9A. Thus, the system 100 can operate in a continuous rather than in a batch mode. At least one adsorbent medium may be used to provide oxygen enriched air into the fuel cell, while another adsorbent medium may be heated and purged to desorb nitrogen adsorbed therein.
  • The operation of the [0044] system 100 as shown in FIG. 3 will now be described in detail. Air from the air source 3 is directed to the inlet selector valve 27, which directs air into at least one of plurality of adsorbent mediums. For example the valve 27 directs the air into the first adsorbent medium 5A but not into the second adsorbent medium 5B. The first adsorbent medium 5A is cooled by the heat transfer fluid in the first heat transfer conduit 9A, and first adsorbent medium 5A selectively adsorbs nitrogen from the air. The oxygen enriched air exits the first adsorbent medium 5A and is selectively directed to the fuel cell through the oxygen enriched air conduits 13A, 13C and the outlet selector valve 29. The inlet selector valve 27 prevents air from flowing from the air source 3 into the second adsorbent medium 5B. Furthermore, the outlet selector valve 29 prevents flow from the second adsorbent medium 5B to the fuel cell. Thus, no oxygen enriched air flows from the second adsorbent medium 5B into the fuel cell.
  • A portion of the oxygen enriched air flows from the first adsorbent medium [0045] 5A through conduit 13A, the connecting conduit 33 and the conduit 13B into the second adsorbent medium 5B. The flow restrictor(s) 35 in the connecting conduit 33 ensure that only a small portion of the oxygen enriched air flows into the second adsorbent medium 5B. This oxygen enriched air from the first adsorbent medium 5A is used as purging air for the second adsorbent medium 5B to purge the nitrogen from the second adsorbent medium 5B. The second adsorbent medium 5B is heated by the heated heat transfer fluid in the conduit 9B to desorb the nitrogen in the second adsorbent medium 5B while the purging air is passing through the second adsorbent medium 5B. The desorbed nitrogen is selectively directed to be vented from the second adsorbent medium but not from the first adsorbent medium by the venting selector valve 31.
  • The heat transfer fluid is directed in the [0046] system 100 shown in FIG. 3 as follows. The heat transfer fluid is passed through a heat sink to cool the heat transfer fluid. The cooled heat transfer fluid is selectively directed to the first adsorbent medium 5A through the “cool inlet” in the heat transfer fluid inlet valve 37B and through conduit 9A.
  • Then, the cooled heat transfer fluid from the first adsorbent medium [0047] 5A is selectively directed through conduit 9A and through the “cool outlet” in the heat transfer fluid outlet valve 39B to the fuel cell. The heat transfer fluid from valve 39B is passed adjacent to the fuel cell to heat the heat transfer fluid.
  • The heated heat transfer fluid is then selectively directed to the second adsorbent medium [0048] 5B through the “hot inlet” in the heat transfer fluid inlet valve 37A and through conduit 9B. Then, the heated heat transfer fluid from the second adsorbent medium 5B is selectively directed through conduit 9B and through the “hot outlet” in the heat transfer fluid outlet valve 39A to the heat sink.
  • The operation of the [0049] system 100 as shown in FIG. 4 will now be described in detail. All of the valves in FIG. 4 are set to provide flow in the opposite direction from FIG. 3. Air from the air source 3 is directed to the inlet selector valve 27 which directs the air into the second adsorbent medium 5B but not into the first adsorbent medium 5A. The second adsorbent medium 5B is cooled by the heat transfer fluid in the second heat transfer conduit 9B, and the second adsorbent medium 5B selectively adsorbs nitrogen from the air. The oxygen enriched air exits the second adsorbent medium 5B and is selectively directed to the fuel cell through the oxygen enriched air conduits 13B, 13C and the outlet selector valve 29. The inlet selector valve 27 prevents air from flowing from the air source 3 into the first adsorbent medium 5A. Furthermore, the outlet selector valve 29 prevents flow from the first adsorbent medium 5A to the fuel cell. Thus, no oxygen enriched air flows from the first adsorbent medium 5A into the fuel cell.
  • A portion of the oxygen enriched air flows from the second adsorbent medium [0050] 5B through conduit 13B, the connecting conduit 33 and the conduit 13A into the first adsorbent medium 5A. The flow restrictor(s) 35 in the connecting conduit ensure that only a small portion of the oxygen enriched air flows into the first adsorbent medium 5A. This oxygen enriched air from the second adsorbent medium 5B is used as purging air for the first adsorbent medium 5A to purge the nitrogen from the first adsorbent medium 5A. The first adsorbent medium 5A is heated by the heated heat transfer fluid in the conduit 9A to desorb the nitrogen in the first adsorbent medium 5A while the purging air is passing through the first adsorbent medium 5A. The desorbed nitrogen is selectively directed to be vented from the first adsorbent medium but not from the second adsorbent medium by the venting selector valve 31.
  • The heat transfer fluid is directed in the [0051] system 100 shown in FIG. 4 as follows. The heat transfer fluid is passed through a heat sink to cool the heat transfer fluid. The cooled heat transfer fluid is selectively directed to the second adsorbent medium 5B through the heat transfer fluid inlet valve 37B and conduit 9B.
  • Then, the cooled heat transfer fluid from the second adsorbent medium [0052] 5B is selectively directed through conduit 9B and the heat transfer fluid outlet valve 39B to the fuel cell. The heat transfer fluid from valve 39B is passed adjacent to the fuel cell to heat the heat transfer fluid.
  • The heated heat transfer fluid is then selectively directed to the first adsorbent medium [0053] 5A through the heat transfer fluid inlet valve 37A and conduit 9A. Then, the heated heat transfer fluid from the second adsorbent medium 5A is selectively directed through conduit 9A and the heat transfer fluid outlet valve 39A to the heat sink.
  • Therefore, [0054] conduits 9A and 9B comprise segments of the same conduit because the heat transfer fluid makes a complete loop through the system 100. However, if desired, the valves 37A, 37B, 39A and 39B may be set such that the heated heat transfer fluid returns to the fuel cell after heating one adsorbent medium, while the cooled heat transfer fluid returns to the heat sink after cooling the other adsorbent medium.
  • It should be noted that the present invention is not limited to the [0055] system 100 illustrated in FIGS. 3 and 4. Several adsorbent mediums (i.e., beds containing adsorbent medium) can be connected in various different ways to achieve the desired oxygen enrichment continuously.
  • FIG. 5 illustrates another [0056] system 200 according to a third preferred aspect of the first embodiment. The system 200 of FIG. 5 is similar to the system 100 of FIGS. 3 and 4, except that the adsorbent mediums 5A, 5B are heated by the hot air emitted by the fuel cell 7, rather than by a heat transfer liquid.
  • As shown in FIG. 5, the air is provided from [0057] inlet 11A into the first adsorbent medium 5A. In the adsorbent medium 5A, nitrogen is adsorbed, and oxygen enriched air is provided through conduits 13A, 13C and valve 29 into the cathode side input of the fuel cell 7. No air is provided into the second adsorbent medium 5B from inlet 11B due to the position of valve 27 in FIG. 5, similar to that of the system 100 illustrated in FIG. 3.
  • The heat transfer conduit [0058] 9 is connected to the cathode side output of the fuel cell 7. The hot air exits the cathode side output of the fuel cell 7 and enters the conduit 9. The hot air then reaches a hot air selector valve 41 which directs the hot air into a first segment 9A or a second segment 9B of the conduit 9. As shown in FIG. 5, the valve 41 is set to direct the hot air into the second segment 9B.
  • Since the [0059] second segment 9B is located adjacent to the second adsorbent medium 5B, the heated air from the fuel cell 7 heats the second adsorbent medium 5B to desorb nitrogen from the adsorbent medium. After the hot air passes through conduit 9B, the air is either vented through vent 43B or reused for some other purpose.
  • When the second adsorbent medium [0060] 5B is used to provide oxygen enriched air into the fuel cell 7, then the position of the valves 27, 31, 29 and 41 is reversed (similar to that shown in FIG. 4), and the first adsorbent medium 5A is heated by the hot air from the fuel cell 7 to desorb the nitrogen from the first adsorbent medium 5A. The hot air is then vented through vent 43A or put to some other use.
  • In FIG. 5, the [0061] fuel cell 7 also contains a fuel input 45 on the anode side and a fuel output 47 on the anode side. In use, the adsorbent mediums 5A, 5B may be cooled by external air or by another heat transfer conduit (not shown in FIG. 5) to adsorb the nitrogen from the air passing from inlets 11A, 11B through the adsorbent mediums 5A, 5B into conduits 13A, 13B. Thus, the heat transfer gas (i.e., hot air) is provided in an open loop in FIG. 5 and the system 200 operates in a continuous mode.
  • In each of these embodiments, conditioning of the incoming air may be valuable. For example, the inlet air may be dried, heated, or cooled depending on its initial state. [0062]
  • It is desirable to select the adsorbent material to optimize both gas separation and rapid heat transfer. The pressure drop through the bed should be minimized in order to reduce the capital and operating costs of the blower. Thus, the particle size, bed geometry, and overall system layout and design may be optimized to minimize the pressure drop. The adsorbent material in different beds may be the same or different depending on the system requirements. [0063]
  • For example, in one case an oxygen enrichment system may consist of three adsorbent beds operating in parallel, similar to the two beds shown in FIG. 2. Each bed will contain 1 kg of AgX zeolite pellets with a standard mesh size of 20×30. The beds will have a parallelipiped geometry and will contain a network of heat transfer surfaces, preferably made of metal foam. [0064]
  • It should be noted that the temperature sensitive adsorption process to enrich the oxygen content of air of the first embodiment is not limited to providing oxygen enriched air to a fuel cell. This process may be used to provide oxygen enriched air for any other suitable use. For example, the efficiency of a combustion process (such as a gas turbine) may increase if the inlet air is oxygen-enriched, as inert nitrogen will not need to be heated. [0065]
  • II. The Second Preferred Embodiment [0066]
  • High powered electrical appliances pose challenges for thermal management. Large electrical power consumers such as co-located computers or fabrication machinery dissipate most of the electrical energy provided as heat. In order to maintain appropriate operating conditions this heat needs to be removed. In conventional arrangements, where electrical power is supplied through the grid, electrical power is required to drive the appliances and to operate a cooling mechanism. Certain distributed power systems offer new perspectives. Power generators such as solid oxide fuel cells provide electrical power and high quality waste heat. This heat can be utilized to drive a cooling device, thereby reducing the electrical power requirement. The inventors have realized that appropriate choice of the equipment involved can provide a system where electrical power requirements and cooling requirements can be ideally matched. [0067]
  • In a second preferred embodiment of the present invention, the inventors have realized that a power generator, which includes a fuel cell, such as a solid oxide fuel cell, a heat pump, and an electrical power consuming appliance, such as a computer, form an ideally matched system with respect to electrical power requirements and cooling requirements. [0068]
  • Solid oxide fuel cells typically generate approximately the same amount of heat as electrical power. This heat is available at elevated temperatures, usually in the range of 250° C. to 1000° C., and is suitable to drive a heat driven heat pump. [0069]
  • There are heat driven heat pumps, which have an efficiency of approximately unity. An efficiency of unity implies that the heat pump can remove the same amount of heat which is supplied to drive the heat pump. It is important to note that the heat streams involved are of different temperature. The heat stream from the fuel cell to the heat driven heat pump is provided at a higher temperature than the heat stream from the cooling load (in this case an electrical appliance) into the heat driven heat pump. [0070]
  • The electrical power supplied by the fuel cell is consumed by an appliance. Part of the electrical power supplied to an appliance is dissipated as heat. A close look at this part of the system reveals that all of the electrical power supplied to the appliance, which is not stored in the appliance or transmitted from the appliance beyond the system boundaries is dissipated. For most appliances, such as computers or machinery, only a small fraction of the power supplied is transmitted beyond system boundaries and most of the electrical energy supplied is dissipated as heat. The dissipated heat needs to be removed in order to avoid excessive temperatures within the appliance. [0071]
  • The inventors have realized that the system described above has the extremely convenient feature of matching cooling loads with electrical loads. The combination of the heat driven heat pump with the solid oxide fuel cell provides electrical supply and cooling capacity matching the requirements of many electrical appliances. Such a system is convenient, because it requires neither additional cooling devices, nor additional electrical power of significance (i.e., over 10% of the total power) to be incorporated. Careful selection of the power generator and the heat driven heat pump can provide matched cooling and heating for a variety of applications. The power generator can also be a combination of a solid oxide fuel cell and a gas turbine, such as a bottoming cycle gas turbine. [0072]
  • Additionally, the amount of cooling and electrical power provided can be adjusted by selecting the appropriate operating conditions for the fuel cell. If for example the fuel cell is supplied with an excess of fuel, more high temperature heat can be created and thereby more cooling power. This adjustment can be especially important in situations where additional heat loads need to be removed. One example for an additional heat load is heating of the conditioned appliance due to high ambient air temperatures (i.e. hot climate zones). [0073]
  • Another preferred option is heating of appliances or thermally conditioned space with the heat pump. For example in cold climate zones heating can be crucial to the operation of appliances or for the personnel operating the appliances. A heat driven heat pump can extremely efficiently provide heating. [0074]
  • A variety of fuels can be used in the power generator. Examples for gaseous fuel are hydrogen, biologically produced gas, natural gas, compressed natural gas, liquefied natural gas, and propane. Liquid fuels can also be used. The system can also be adapted to solid fuels. [0075]
  • FIG. 6 schematically illustrates the system of the second preferred embodiment. The system contains an [0076] electrical power generator 2, a heat driven heat pump 4, an appliance 6, and a heat sink 8. The electrical power generator 2 can be a solid oxide fuel cell. It can also be a solid oxide fuel cell combined with a gas turbine. Other power generators, such as molten carbonate fuel cells, which also provide high temperature heat in addition to electrical power, can also be used. The heat driven heat pump 4 can be an absorbtion chiller, such as a LiBr-Water or an ammonia-water heat pump. Heat driven heat pumps use high temperature heat to provide cooling (i.e. absorb heat at a low temperature), and reject heat at an intermediate temperature. Compared to conventional Rankine-cycle cooling devices, they require only a small amount of electrical or mechanical power. A description of heat driven heat pumps can be found in Bernard D. Woods, “Applications of Thermodynamics”, Waveland Press, Inc., Prospect Heights, Ill., Second Edition, 1991, incorporated herein by reference.
  • Another class of heat driven heat pumps suitable for this embodiment is adsorption heat pumps. In an adsorption heat pump the refrigerant, which is usually a gas, interacts with a solid. Adsorption and desorption of the refrigerant on/from the solid provide pressurization of the refrigerant. High pressure desorption of the refrigerant is accomplished using high temperature heat. In the high-pressure portion of the refrigerant loop, heat is rejected and in the low pressure portion heat is absorbed. Adsorption heat pumps can be realized as solid state devices without the need to handle liquids. This can be advantageous for example in environments where handling of the liquids commonly involved in absorption heat pumps is too hazardous. Environmentally friendly gases/vapors can be used in the adsorption heat pump. [0077]
  • The [0078] appliance 6 is a device that consumes electrical power for any purpose and generates heat (appliance cooling load), mostly as a parasitic loss, which needs to be removed. One preferred example for this appliance is a computer or a cluster of computers co-located in a data center.
  • A [0079] heat sink 8 for the system can be a large body of solid, liquid or gas. For example the heat sink can comprise, a cooling tower, ambient atmospheric air, soil, or a stream of water.
  • Also shown in FIG. 6 are the energies exchanged between the subsystems. The [0080] electrical power 12 provided by the electrical power generator 2 to the appliance 6 can be transferred using electrical wire, but other electrical power transfer mechanisms can also be used. The high temperature heat 10 is generated by the electrical power generator 2 and consumed by the heat driven heat pump 4. The high temperature heat 10 can be transported with a pumped fluid loop, such as a liquid loop, in which the fluid absorbs heat in or near the electrical power generator 2 and releases heat to the heat driven heat pump 4. Generally, this heat transfer can be accomplished by any heat transfer mechanism (i.e. conduction, convection, radiation, or any combination thereof). The cooling loop can also consist of gas or vapor coolant and/ or solid beds. The appliance cooling load 14 is the amount of heat generated by the appliance 6, which needs to be removed by the heat pump 4. Heat is absorbed at or near the appliance 6 and transported to the heat driven heat pump 4. A liquid pumped loop or a stream of gas can be used to absorb the cooling load 14 from the appliance 6 and transport it to the heat driven heat pump 4. The moderate temperature heat 16 is the heat transferred from the heat driven heat pump 4 to the heat sink 8. Here again, convection, conduction, radiation, or any combination of these heat transfer mechanisms can be used to transport this heat. One possible implementation is atmospheric air blown through a heat exchanger inside the heat driven heat pump and released back to ambient. All three heat transfers (10, 14, 16) can be realized with a single or multiple heat streams. In the case of a LiBr-water heat driven heat pump, the moderate temperature heat 16 from the heat driven heat pump 4 to the heat sink 8 is commonly realized with two transport loops.
  • An example for the heat transfer loop from the heat driven [0081] heat pump 4 to the heat sink 8 is a pumped loop with tubes wrapped around the part of the heat driven heat pump 4 that requires cooling and coils of tubes buried in the soil. Another example is a blower sucking in ambient air, blowing it over the surface that needs to be cooled and a conduit releasing the warm air back to ambient.
  • The subsystem formed by the [0082] electrical power generator 2 and the heat driven heat pump 4 is illustrated in FIG. 7 for the case where a high temperature fuel cell is used as the electrical power generator 2. The fuel cell 68 is preferably a high temperature fuel cell, such as a solid oxide fuel cell.
  • Fuel is delivered to the fuel cell with the help of a [0083] fuel blower 18, which can also be a compressor. For liquid fuels, the blower 18 is replaced by a pump. An optional fuel preconditioner 104 preprocesses the fuel. For example this device can remove contaminants detrimental to the function of the power generator, such as sulfur. Another possible function for the fuel preconditioner 104 is prereformation and/ or reformation.
  • The [0084] fuel preheater 22 brings the fuel to fuel cell operating temperature. This preheater can be external to or an integral part of the fuel cell 68. It can be contained in one single or multiple devices. For a liquid fuel, the fuel preheater 22 evaporates the liquid fuel. For a gaseous fuel, the fuel preheater 22 can be a finned heat exchanger. A fuel preconditioner 104 can also be implemented after the fuel preheater 22 or integrated with the fuel preheater 22, or integral to fuel cell 68.
  • The [0085] fuel preheat 54 is the heat required raise the temperature of the input fuel to the fuel cell operating temperature. The fuel intake conduit 34 provides a path for the fuel from the fuel blower 18 to the fuel preheater 22. It may or may not have an intermediate fuel preconditioner 104. The fuel delivery conduit 36 provides a path for the fuel from the fuel preheater 22 to the fuel cell 68.
  • The [0086] oxidizer blower 20 drives air or any other suitable oxidizer toward the fuel cell 68. The oxidizer intake conduit 42 provides a transport path for the oxidizer between the oxidizer blower 20 and the oxidizer preheater 24. An optional oxidizer preconditioner 106 preprocesses the oxidizer flow. Examples of the preconditioner 106 include filters, and oxygen enrichment devices. The preconditioner heat 11A is heat required to operate this optional device. One example for one component of the preconditioner 106 is an oxygen enrichment device utilizing temperature swing adsorption, as described in the first preferred embodiment. The oxidizer preconditioner 106 can also be installed upstream of the oxidizer blower 20. The oxidizer preheater 24 brings the input oxidizer to fuel cell operating temperature using the oxidizer preheat 62. The oxidizer preheater 24 can be contained in single or multiple devices. In one preferred embodiment, the oxidizer is partially preheated in oxidizer preheater 24 and picks up additional heat inside the fuel cell 68, thereby cooling the fuel cell 68. One example for the oxidizer preheater 24 is a finned heat exchanger. The oxidizer delivery conduit 44 transports the oxidizer from the oxidizer preheater 24 to the fuel cell 68.
  • In the [0087] fuel cell 68, the fuel and the oxidizer are electrochemically reacted. This reaction produces electrical energy 12 and high temperature heat. The fuel cell high temperature heat 58 represents the part of the heat generated by the fuel cell which is harnessed for further use and not removed by the exhaust or the depleted oxidizer. Not all of the heat generated by the fuel cell can be harnessed and transported to other devices.
  • The fuel cell [0088] high temperature heat 58 can be utilized for various purposes. This heat can be used for the fuel preheat 54, the oxidizer preheat 62, preconditioner heat 11A, or the heat driven heat pump high temperature input heat 10. The fuel cell high temperature heat 58 can be directed to any combination of these heat consumers (10, 54, 62,11A). One possibility for harnessing the fuel cell high temperature heat 58 is a gas cooling loop, separate from the oxidizer flow loop to the fuel cell.
  • The fuel [0089] cell outlet conduits 38 and 46 transport the electrochemical reaction products. If the fuel cell 68 is a solid oxide fuel cell, then the exhaust conduit 38 transports reacted fuel and the outlet oxidizer conduit 46 transports oxygen depleted oxidizer. The fuel outlet cooler 28 extracts the exhaust cooling heat 56 from the exhaust stream. The fuel outlet cooler 28 can be one or multiple devices and can be partly or fully integrated with the fuel cell 68. One example for the fuel outlet cooler 28 is a finned heat exchanger. The exhaust cooling heat 56 can be used for the fuel preheat 54, the oxidizer preheat 62, preconditioner heat 11A, or the heat driven heat pump high temperature input heat 10. The exhaust cooling heat 56 can be directed to any combination of these heat consumers (10, 54, 62, 11A).
  • The oxidizer outlet cooler [0090] 26 extracts the oxidizer cooling heat 60 from the outlet oxidizer stream. The oxidizer outlet cooler 26 can be one or multiple devices and can be partly or fully integrated with the fuel cell 68. One example for the oxidizer outlet cooler is a finned heat exchanger. The oxidizer cooling heat 60 can be used for the fuel preheat 54, the oxidizer preheat 62, preconditioner heat 11A, or the heat driven heat pump high temperature input heat 10. The oxidizer cooling heat 60 can be directed to any combination of these heat consumers (10, 54, 62, 11A).
  • The fuel outlet (i.e., exhaust) [0091] conduit 38 and the oxidizer outlet (i.e., exhaust) conduit 46 deliver fuel exhaust and oxygen depleted oxidizer to the optional burner 30. In the burner 30, these two gas streams are chemically reacted, generating the burner high temperature heat 48. The chemical reaction can be initiated by an optional catalyst material.
  • The burner [0092] high temperature heat 48 can be provided to the fuel preheat 54, the oxidizer preheat 62, preconditioner heat 11A, or the heat driven heat pump high temperature input heat 10. The burner high temperature heat 48 can be directed to any combination of these heat consumers (10, 54, 62,11A). One preferred example of transport of the burner high temperature heat 48 is direct integration of the burner with the consumer (i.e. heat transfer by conduction to the consumer). Another preferred example for this heat transport is a pumped fluid loop.
  • The [0093] burner exhaust conduit 50 transports the reaction products from the burner 30 to the optional burner exhaust heat exchanger 32. In the burner exhaust heat exchanger 32 the burner exhaust heat 64 is extracted from the burner reaction products. One example for the burner exhaust heat exchanger 32 is a finned heat exchanger.
  • The [0094] burner exhaust heat 64 can be provided to the fuel preheat 54, the oxidizer preheat 62, preconditioner heat 11A, or the heat driven heat pump high temperature input heat 10. The burner exhaust heat 64 can be directed to any combination of these heat consumers (10, 54, 62,11A). The burner heat exchanger exhaust conduit 102 transports the burner exhaust out of the system (preferably vented to ambient or into an exhaust post-processor).
  • The heat driven [0095] heat pump 4 is driven by the high temperature heat 10. After using heat from the high temperature heat 10 the heat driven heat pump 4 vents one heat stream in the heat pump low-temperature outflow 16A. The appliance cooling load 14 from appliance 6 is removed by the cooling stream 16B. The high temperature heat 10 can be provided by the fuel cell high temperature heat 58, the exhaust cooling heat 56, the oxidizer cooling heat 60, the burner high temperature heat 48, or the burner exhaust heat 64. The high temperature heat 10 can also be provided by any combination of these heat sources (48, 56, 58, 60, 64).
  • One preferred implementation for the [0096] appliance cooling load 14 and the heat 16B is ambient air driven by a blower into the heat driven heat pump 4, cooled below ambient temperature in the heat driven heat pump, and then directed to the appliance that requires cooling. At the appliance the cool air picks up the cooling load 14 and is heated. The heated air is vented back to ambient.
  • One preferred embodiment of the system shown in FIG. 7 is presented in FIG. 8A. The system shown in FIG. 8A follows the same outline presented for FIG. 7. FIG. 8A includes one preferred routing of the heat streams shown in FIG. 7. The [0097] fuel preheat 54 is provided by the fuel exhaust cooling heat 56. Optionally, the fuel can pick up additional heat in the fuel cell. The heat transfer from exhaust cooling heat 56 to fuel preheat 54 can be realized in a heat exchanger, for example a finned heat exchanger. One example of this configuration is to combine heat exchangers 22 and 28 as a single component. Depending on the choice of fuel, water vapor can be transferred from the exhaust to the input fuel. This water transport can be integrated into a heat exchanger or it can be realized with a separate device.
  • The [0098] oxidizer preheat 62 is provided partly by the oxidizer exhaust cooling heat 60. The remainder of the heat needed to bring the oxidizer to fuel cell operating temperature is absorbed in the fuel cell, thereby removing all of the high temperature heat from the fuel cell without an additional heat transfer loop. The heat transfer from oxidizer exhaust cooling heat 60 to oxidizer preheat 62 can be realized in a heat exchanger, for example a finned heat exchanger. One example of this configuration is to combine heat exchangers 24 and 26 as a single component. The burner high temperature heat 48 is not immediately extracted. Instead, it is extracted together with burner exhaust heat 64. The burner exhaust heat 64 is directed to the high temperature heat 10, which provides the necessary heat to actuate the heat driven heat pump 4. The heat transfer from the burner exhaust heat 64 to the heat driven heat pump 4 can be realized with a heat exchanger incorporated in the heat driven heat pump 4. Thus the burner exhaust heat exchanger 32 is combined with the heat exchanger in the heat pump 4 to form a single component. This heat exchanger can be a finned heat exchanger. The cooling load 14 can be extracted from the appliance 6 by a cool air stream provided by the heat driven heat pump 4, which is driven with a cooling air-blower 72 through cooling air inlet duct 74 directed to the appliance with a cooling air conduit 76.
  • Table 1 presents an energy balance for a 100 kW electrical power system based on FIG. 8A. The naming convention, where applicable, is consistent with FIG. 8A. [0099]
    TABLE 1
    typical
    range example
    item low high layout units
    DC electrical power output 12 0.005 100 0.1  [MW]
    Fuel cell electrical efficiency 35% 75% 50%
    (fraction of higher heating value of fuel
    supplied, which is available as DC
    electrical power)
    Fuel cell fuel conversion efficiency 50% 90% 80%
    (fraction of fuel supplied,
    which is oxidized in fuel cell)
    Heat leakage fuel cell  5% 50% 20%
    (fraction of heat generated in fuel cell
    which is not harnessed)
    Coefficient of performance heat driven 0.6   1.5 1.2 
    heat pump (fraction of high temperature
    heat
    10, which is available as cooling
    power 14)
    Fuel cell efficiency 62.5%  
    (fraction of heat of fuel oxidized in fuel
    cell, which is available as DC electrical
    power)
    High temperature heat generated by fuel 0.060 [MW]
    cell
    Heat leakage from fuel cell (heat not 0.012 [MW]
    harnessed)
    Burner high temperature heat 60 0.040 [MW]
    High temperture input heat 10 0.088 [MW]
    Cooling power available from heat 0.106 [MW]
    driven heat pump
  • FIG. 8B illustrates another preferred aspect of the second embodiment of this invention. The system illustrated in FIG. 8B shows an alternative preferred routing of the heat streams shown in FIG. 7. The system depicted in FIG. 8B is similar to the system depicted in FIG. 8A, with the exception that the [0100] oxidizer cooling heat 60 is provided to the heat exchanger 4 as the high temperature heat 10, and the burner exhaust heat 64 is provided to the oxidizer preheater 24 as oxidizer preheat 62.
  • Thus, the [0101] oxidizer outlet conduit 46 is provided into the heat exchanger of the heat pump 4 and then into the burner 30, while the burner exhaust conduit 50 is provided into the burner exhaust heat exchanger 32. Both the heat transfer from the oxidizer cooling heat 60 to the high temperature heat 10 and the burner exhaust heat 64 to the oxidizer preheat 62 can be realized with heat exchangers. Thus, the oxidizer preheater 24 and the burner exhaust heat exchanger 32 are combined as a single component and comprise portions of the same heat exchanger 24/32. Likewise, the outlet oxidizer cooler 26 and the heat exchanger portion of the heat pump 4 are combined as a single component and comprise a portion of the same heat exchanger.
  • FIG. 8C illustrates another preferred aspect of the second embodiment of this invention. The system illustrated in FIG. 8C shows an alternative preferred routing of the heat streams shown in FIG. 7. The system depicted in FIG. 8C is similar to the system depicted in FIG. 8A, but differs by a cross-over of the exhaust fuel and oxidizer paths. In FIG. 8C, the [0102] fuel outlet conduit 38 is provided into the oxidizer outlet cooler 28, while the oxidizer outlet conduit 46 is provided into the fuel outlet cooler 26. Thus, the exhaust cooling heat 56 is provided as oxidizer preheat 62 and oxidizer cooling heat 60 is provided as fuel preheat 54. Both heat transfers can be realized with heat exchangers. Thus, the oxidizer preheater 24 and the fuel outlet cooler 28 are combined as a single component and comprise portions of the same heat exchanger 24/28. Likewise, the outlet oxidizer cooler 26 and the fuel preheater 22 are combined as a single component and comprise a portion of the same heat exchanger 22/26.
  • FIG. 9 shows another preferred embodiment of the system depicted in FIG. 6. The main difference between FIG. 7 and FIG. 9 is the addition of a gas turbine driven electrical power generator. The gas turbine can utilize the high temperature heat from the fuel cell to generate additional electrical energy and thereby further increase the electrical efficiency of the electrical power generator. High temperature waste heat is still available to drive a heat driven heat pump and thereby form a complementary system, which can provide matched electrical power and cooling. The increase of efficiency of the power generator implies that less high temperature heat per electrical power generated is available. Such an embodiment is used preferentially when the electrical load requirements are greater than the cooling load requirements and there are no environmental and permitting issues against the use of gas turbines. This embodiment can also be used with a heat driven heat pump of higher efficiency such as to complete the balance between the electrical and thermal loads in the system described above. [0103]
  • In FIG. 9 the fuel is compressed and transported into the system by the [0104] fuel compressor 80. A fuel compressor inlet conduit 82 delivers the fuel to the fuel compressor 80. For a liquid fuel, a fuel pump can be used instead of the fuel compressor 80. An optional fuel preconditioner 104 preprocesses the fuel. For example this device can remove contaminants detrimental to the function of the power generator, such as sulfur. Another possible function for the fuel preconditioner 104 is prereformation or reformation.
  • The [0105] fuel preheater 22 brings the fuel to fuel cell operating temperature. If the fuel is provided as a liquid, the fuel is evaporated in the fuel preheater 22. This preheater can be external to or an integral part of the fuel cell 68. It can be contained in one single or multiple devices. The fuel preheat 54 is the heat required to bring the fuel to fuel cell operating temperature. The fuel intake conduit 34 provides a path for the fuel from the fuel compressor 80 to the fuel preheater 22. The fuel delivery conduit 36 provides a path for the fuel from the fuel preheater 22 to the fuel cell 68.
  • The [0106] oxidizer compressor 84 drives air or any other suitable oxidizer to the fuel cell 68. The oxidizer compressor inlet conduit 86 delivers the oxidizer to the oxidizer compressor 84. An optional oxidizer preconditioner 106 preprocesses the oxidizer flow. Examples of the preconditioner 106 include filters, and oxygen enrichment devices. The preconditioner heat 11A is heat required to operate this optional device. One example for one component of the preconditioner 106 is an oxygen enrichment device utilizing temperature swing adsorption. The oxidizer preconditioner 106 can also be installed downstream of the oxidizer compressor 84. The oxidizer intake conduit 42 provides a transport path for the oxidizer between the oxidizer compressor 84 and the oxidizer preheater 24. The oxidizer preheater 24 brings the input oxidizer to fuel cell operating temperature using the oxidizer preheat 62. The oxidizer preheater 24 can be contained in a single or multiple devices. In one preferred embodiment, the oxidizer is partially preheated in oxidizer preheater 24 and picks up additional heat inside the fuel cell 68, thereby cooling the fuel cell 68. The oxidizer delivery conduit 44 transports the oxidizer from the oxidizer preheater 24 to the fuel cell 68.
  • In the [0107] fuel cell 68, the fuel and the oxidizer are electrochemically reacted. This reaction produces electrical energy 12A high temperature heat 58.
  • The oxidizer outlet cooler [0108] 26 extracts the oxidizer cooling heat 60 from the outlet oxidizer stream. The outlet oxidizer cooler 26 can be one or multiple devices and can be partly or fully integrated with the fuel cell 68. The fuel outlet cooler 28 extracts the exhaust cooling heat 56 from the exhaust stream. The fuel outlet cooler 28 can be one or multiple devices and can be partly or fully integrated with the fuel cell 68. One example for the coolers 26, 28 is a finned heat exchanger.
  • The [0109] fuel exhaust conduit 38 and the oxidizer outlet conduit 46 deliver fuel exhaust and oxygen depleted oxidizer to the optional burner 30. In the burner 30 these two gas streams are chemically reacted, generating the burner high temperature heat 48.
  • The burner [0110] high temperature heat 48 can be provided to the fuel preheat 54, the oxidizer preheat 62, the preconditioner heat 11A, or the high temperature heat 10. The burner high temperature heat 48 can be directed to any combination of these heat consumers (10, 11A, 54, 62).
  • The [0111] burner exhaust conduit 50 transports the reaction products from the burner 30 to the optional burner exhaust heat exchanger 32. In the burner exhaust heat exchanger the burner exhaust heat 64 is extracted from the burner reaction products.
  • The [0112] burner exhaust heat 64 can be provided to the fuel preheat 54, the oxidizer preheat 62, the preconditioner heat 11A, or the high temperature heat 10. The burner exhaust heat 64 can be directed to any combination of these heat consumers (10, 11A, 54, 62).
  • The [0113] turbine inlet conduit 88 transports the burner exhaust to the turbine 90. A mechanical coupling 92 transmits mechanical energy from the turbine 90 to the oxidizer compressor 84, the fuel compressor 80, and/or the electrical generator 94. If desired, the compressors may be actuated by another source of mechanical energy and/or electrical power. The electrical generator 94 generates additional electrical power 12B.
  • The [0114] turbine outlet conduit 96 transports the turbine exhaust to the optional turbine exhaust heat exchanger 98. In the turbine exhaust heat exchanger the turbine exhaust heat 100A is extracted from the gas flow. The turbine exhaust heat 100A can be provided to the fuel preheat 54, the oxidizer preheat 62, the preconditioner heat 11A, or the high temperature heat 10. The turbine exhaust heat 100A can be directed to any combination of these heat consumers (10, 11A, 54, 62). The exhaust conduit 102 transports the exhaust gases out of the system (preferably vented to ambient or into an exhaust post-processor).
  • The heat driven [0115] heat pump 4 is driven by the high temperature heat 10. After utilizing heat from the high temperature heat 10, the heat driven heat pump 4 vents one heat stream in the moderate temperature heat 16A. The appliance cooling load 14 from appliance 6 is removed by the cooling stream 16B. The high temperature heat 10 can be provided by the fuel cell high temperature heat 58, the exhaust cooling heat 56, the oxidizer cooling heat 60, the burner high temperature heat 48, the burner exhaust heat 64, or the turbine exhaust heat 100A. The high temperature heat 10 can also be provided by any combination of these heat sources (46, 56, 58, 60, 64, 100A).
  • One preferred embodiment of the system shown in FIG. 9 is presented in FIG. 10A. The system shown in FIG. 10A follows the same outline presented for FIG. 9. FIG. 10A includes one preferred routing of the heat streams involved. The [0116] fuel preheat 54 is provided by the exhaust cooling heat 56. Optionally, the fuel can pick up additional heat in the fuel cell. The heat transfer from exhaust cooling heat 56 to fuel preheat 54 can be realized in a heat exchanger, for example a finned heat exchanger 22/28. Depending on the choice of fuel, water vapor can be transferred from the exhaust to the input fuel. This water transport can be integrated into a heat exchanger or it can be realized with a separate device. The oxidizer preheat 62 is provided partly by the oxidizer cooling heat 60. The remainder of the heat needed to bring the oxidizer to fuel cell operating temperature is absorbed in the fuel cell, thereby removing all of the high temperature heat from the fuel cell without an additional heat transfer loop. The heat transfer from oxidizer cooling heat 60 to oxidizer preheat 62 can be realized in a heat exchanger, for example a finned heat exchanger 24/26.
  • The burner [0117] high temperature heat 48 together with the high temperature heat from the fuel cell carried by the burner exhaust gas 64 is first used to drive the turbine 90. The remaining heat after the turbine is used as high temperature heat 10 to drive the heat driven heat pump 4.
  • The heat transfer from the [0118] turbine exhaust heat 100A to the heat driven heat pump 4 can be realized with a heat exchanger incorporated in the heat driven heat pump 4. Thus the turbine exhaust heat exchanger 98 and the heat exchanger portion of the heat pump 4 are combined as a single heat exchanger. This heat exchanger can be a finned heat exchanger. The cooling load 14 can be absorbed from the appliance 6 by a cool air stream provided by the heat driven heat pump 4, which is driven with a cooling air blower 72 through cooling air inlet duct 74 directed to the appliance with a cooling air conduit 76.
  • FIG. 10B illustrates another preferred aspect of the second embodiment of this invention. The system illustrated in FIG. 10B shows an alternative preferred routing of the oxidizer stream shown in FIGS. 9 and 10A. The system depicted in FIG. 10B is similar to the system depicted in FIG. 10A, with the exception of the oxidizer routing. In the system of FIG. 10B, the [0119] gas turbine 90 and the fuel cell 68 are fed with separate oxidizer streams. An oxidizer blower 20 is used for the oxidizer supply for the fuel cell. This blower can also be a compressor. The compressor 84 delivers oxidizer to the burner 30 via conduit 45A. The unreacted fuel from the fuel cell is combusted in the burner. The burner exhaust drives the turbine 90. The advantage of this system is that a higher oxygen content oxidizer is supplied to the burner. This improves the combustion process in the burner and subsequently improves the turbine operation.
  • FIG. 10C illustrates another preferred aspect of the second embodiment of this invention. The system illustrated in FIG. 10C shows an alternative preferred routing of the heat streams shown in FIG. 9. The system in FIG. 10C is differs from the system in FIG. 10A by the sequence of heat usage from the oxidizer. In FIG. 10C the oxidizer leaving the [0120] fuel cell 68 first delivers the oxidizer cooling heat 60 to the high temperature input heat 10 in the heat pump 4, and then enters the burner 30. The oxidizer preheat 62 is provided by the turbine exhaust heat 100A. Thus, the oxidizer preheater 24 and the turbine exhaust heat exchanger 98 are combined as a single component and comprise portions of the same heat exchanger 24/98. Likewise, the outlet oxidizer cooler 26 and the heat exchanger portion of the heat pump 4 are combined as a single component and comprise a portion of the same heat exchanger.
  • The system in FIG. 10C relates similarly to FIG. 10A as the system in FIG. 8B relates to the system in FIG. 8A. The system in FIG. 10C can also incorporate the use of separate oxidizers for the fuel cell and the [0121] burner 30, as shown in FIG. 10B. It may be advantageous to provide separate oxidizer streams for the fuel cell 68 and the turbine 90.
  • FIG. 10D illustrates another preferred aspect of the second embodiment of this invention. The system illustrated in FIG. 10D shows an alternative preferred routing of the heat streams shown in FIG. 9. The system depicted in FIG. 10D is similar to the system depicted in FIG. 10A, but differs by the routing of the heat fluxes. In FIG. 10D, the [0122] fuel preheat 54 is provided by the turbine exhaust heat 100A, while the high temperature heat 10 is provided by the fuel exhaust cooling heat 56. Thus, the turbine outlet conduit 96 is provided into the turbine exhaust heat exchanger 98, while the fuel cell fuel outlet conduit 38 is provided into the heat exchanger portion of the heat pump 4. Thus, the turbine exhaust heat exchanger 98 and the fuel preheater 22 are combined as a single component and comprise portions of the same heat exchanger 22/98. Likewise, the outlet fuel cooler 28 and the heat exchanger portion of the heat pump 4 are combined as a single component and comprise a portion of the same heat exchanger. This routing can be applied to any of the systems of FIGS. 10A, 10B and 10C previously discussed.
  • FIGS. [0123] 6 to 10D present the basic layouts of the components of the systems of the preferred aspects of the second embodiment. These components can also be combined in a large number of other ways not shown in these Figures. Any component or combination of components shown in one figure may be used in a system shown in any other figure. For example, the cross over of the fuel cell fuel and oxidizer exhaust paths shown in FIG. 8C can be applied to the systems shown in FIGS. 8A, 8B, 10A, 10B, 10C, 10D, as well as combinations of these systems.
    Parts List
    electrical power generator 2
    heat driven heat pump 4
    appliance 6
    heat sink 8
    high temperature heat 10
    preconditioner input heat   11A
    electrical power 12
    appliance cooling load 14
    moderate temperature heat 16
    heat pump low-temperature outflow   16A
    low temperature outflow   16B
    fuel blower
    18
    oxidizer blower 20
    fuel preheater 22
    oxidizer preheater 24
    oxidizer outlet cooler 26
    fuel outlet cooler 28
    burner 30
    burner exhaust heat exchanger 32
    fuel intake conduit 34
    fuel delivery conduit 36
    fuel cell fuel outlet conduit(s) 38
    oxidizer intake conduit 42
    oxidizer delivery conduit 44
    conduit from oxidizer compressor to burner   45A
    fuel cell oxidizer outlet conduit(s) 46
    burner high temperature heat 48
    burner exhaust conduit 50
    fuel preheat 54
    fuel exhaust cooling heat 56
    fuel cell high temperature heat 58
    oxidizer exhaust cooling heat 60
    oxidizer preheat 62
    burner exhaust heat 64
    fuel cell 68
    appliance cooling load 70
    cooling air blower 72
    cooling air conduit 74
    cooling air outlet 76
    burner exhaust cooler 78
    fuel compressor 80
    fuel compressor inlet conduit 82
    oxidizer compressor 84
    oxidizer compressor inlet conduit 86
    turbine inlet conduit 88
    turbine 90
    mechanical coupling 92
    electrical generator 94
    turbine oulet conduit 96
    turbine exhaust heat exchanger 98
    turbine exhaust heat 100A
    exhaust conduit
    102 
    fuel cell electrical power   12A
    generator electrical power output   12B
    fuel preconditioner
    104 
    oxidizer preconditioner 106 
  • III. The Third Preferred Embodiment [0124]
  • In one prior art solid [0125] oxide fuel cell 100, the ceramic electrolyte 101 is corrugated, as shown in FIG. 11. While the whole electrolyte 101 is bent or corrugated, its major surfaces 103, 105 are smooth or uniform. Thus, the electrolyte 101 has the same thickness along its length. However, the imaginary center line 107 running along the length of the electrolyte 101 significantly deviates from an imaginary straight line 109. The anode 111 and cathode 113 are formed on the uniform surfaces 103, 105 of the electrolyte 101. Such a corrugated electrolyte 101 is difficult to manufacture and even more difficult to properly integrate in a fuel cell stack containing a plurality of fuel cells.
  • The present inventors have realized that if at least a portion of at least one surface of the electrolyte is made non-uniform, then several advantages may be realized. The oxygen diffusion through an electrolyte in a solid oxide fuel cell proceeds between so-called “three phase boundaries.” These three phase boundaries are electrolyte grain boundary regions at the boundary of an electrode (i.e., cathode or anode) and electrolyte, as shown in FIG. 12. Diffusing oxygen makes up the third “phase.” If the active portions of one or both major surfaces of the electrolyte are made non-uniform, then the surface area between the electrolyte and the electrode contacting the non-uniform surface is increased. The “active portion” of the electrolyte is the area between the electrodes that generates the electric current. In contrast, the peripheral portion of the electrolyte is used for attaching the electrolyte to the fuel cell stack and may contain fuel and oxygen passages. The increased surface area results in more three phase boundary regions, which allows more oxygen to diffuse through the electrolyte. This increases the power density (i.e., watts per cm[0126] 2) of the fuel cell and decreases the cost per watt of the fuel cell.
  • FIG. 13 illustrates a solid [0127] oxide fuel cell 200 containing a ceramic electrolyte 201 having at least one non-uniform surface portion, according to a first preferred aspect of the third embodiment. The at least one non-uniform surface in the first preferred aspect is a textured surface. Preferably, two opposing major surfaces 203, 205 are textured. A textured surface 203, 205 contains a plurality of protrusions (i.e., bumps, peaks, etc.) 206 having a height 208 that is 5% or less, preferably 1% or less of an average electrolyte thickness 209. The height and width of the protrusions 206 is exaggerated in FIG. 13 for clarity. The protrusions 206 may have any desired shape, such as rectangular, polygonal, triangular, pyramidal, semi-spherical or any irregular shape. Preferably, only the active portions 210 of the opposing major surfaces 203, 205 are textured, while the peripheral portions 202 of the surfaces 203, 205 are not textured. However, if desired, the entire major surfaces 203, 205 may be textured. For example, in adhesive or compression seals, where the integrity of the seal increases with the area of the contact surfaces, texturing the peripheral portions can increase the seal integrity and/ or reduce the “non-active” peripheral area of the fuel cell.
  • In contrast to the corrugated electrolyte of FIG. 11, the electrolyte shown in FIG. 13 is substantially flat. The [0128] imaginary center line 207 running along the length of the electrolyte 201 does not significantly deviate from an imaginary straight line. While the whole electrolyte 201 is substantially flat, its major opposing surfaces 203, 205 are non-uniform and textured. The anode 211 and cathode 213 are formed on the textured surfaces 203, 205 of the electrolyte 201. The substantially flat electrolyte is advantageous because it is easier to manufacture, because it is easier to integrate into a fuel cell stack and because it is more durable than a corrugated electrolyte. However, if desired, the textured surface(s) may be located on a non-flat or corrugated electrolyte.
  • The electrolyte, anode and cathode may be made of any appropriate materials. Preferably, the electrolyte comprises a yttria stabilized zirconia (YSZ) ceramic. The cathode preferably comprises a Perovskite ceramic having a general formula ABO[0129] 3, such as LaSrMnO3 (“LSM”). The anode preferably comprises a metal, such as Ni, or a metal containing cermet, such as a Ni—YSZ or Cu—YSZ cermet. Other suitable materials may be used if desired.
  • The non-uniform surface of the electrolyte may be formed by any suitable method. Preferably, the non-uniform surface is made by providing a ceramic green sheet and patterning at least a portion of at least one surface of the green sheet to form at least a non-uniform portion of the at least one surface. The green sheet may then be sintered (i.e., fired or annealed at a high temperature) to form the ceramic electrolyte. It should be noted that the term “green sheet” includes a green tape or a sheet of finite size. Preferably both sides of the green sheet are patterned to form two opposing non-uniform surface portions of the green sheet. [0130]
  • Another preferred aspect of the third embodiment of the present invention is directed to a composite electrolyte with a textured interface. FIG. 14 illustrates a prior art composite electrolyte, while FIGS. 15 and 16 illustrate a composite electrolyte with a textured interface according to the third preferred embodiement. It can be advantageous to fabricate the electrolyte not from one single material, which is typically yttria stabilized zirconia (YSZ), but to use several layers of materials. One example for composite electrolyte is a samaria-doped ceria (SDC) electrolyte coated with YSZ on one or both sides. SDC has the advantage over YSZ to provide higher ionic conductivity. However, the application of SDC is limited by its ability to withstand low oxygen partial pressures. At low oxygen partial pressures SDC can be reduced, lose its ionic conductivity in part or in whole and thereby cause a critical failure in a solid oxide fuel cell. YSZ has a lower ionic conductivity, which implies higher electrical losses within this material, but it can withstand lower oxygen partial pressures compared to SDC. Also, SDC displays electron conductivity at elevated temperatures, which is detrimental to the performance of a fuel cell. A layer of YSZ next to SDC can effectively suppress electron conduction, since YSZ is a very weak electron conductor. [0131]
  • FIG. 14 shows a prior [0132] art YSZ electrolyte 300, which is coated or laminated with a layer of SDC 305. One example is to use the SDC on the cathode side of the solid oxide fuel cell, which is not exposed to the reacting fuel, and thereby not exposed to low oxygen partial pressure, while the YSZ is used on the anode side.
  • The high oxygen ion conductivity in SDC can create a rate limiting step at the interface between SDC and YSZ. The losses at the interface between the two materials can be reduced by increasing the surface area of the interface. An increase in interface area can be accomplished by texturing the interface. FIG. 15 shows a cross section of a composite electrolyte with a textured internal interface. Here a textured layer of [0133] SDC 315 is attached to a layer of YSZ 310.
  • The combination of YSZ and SDC is one example where a textured interface can be used. Other material combination can also be used with textured interfaces. The composite electrolyte can consist of two layers as shown in FIG. 15 or of three or [0134] more layers 310, 315, 320 with at least one, and preferably more than one textured interface 303, 305 as shown in FIG. 16.
  • Textured interfaces can be formed by any suitable method. One method is the lamination of two textured matching surfaces. Another method is the application of the second layer onto a textured surface of the first material, for example by tape casting or by screen printing. In a preferred example, the SDC is provided as a mechanically supporting substrate with a thickness of about 50 to 200 micrometers, preferably about 100 micrometers and the YSZ is deposited on the substrate as a thin protective layer of about 10 to 50 micrometers, preferably about 20 micrometers. In this case, the surface texture can have a thickness of about 10 micrometers. However, texturing on larger and smaller length scales is also possible. [0135]
  • The textured internal interfaces (i.e., interface surfaces) illustrated in FIGS. 15 and 16 can be formed on composite electrolytes also having textured [0136] outer surfaces 203, 205 (i.e., surfaces that contact the electrodes). One or both of the outer composite electrolyte surfaces can be textured.
  • Additional layers that offer superior mechanical, thermal, and/or electrical properties may be added to composite or single layer electrolytes to provide improved superior mechanical, thermal, and/or electrical properties compared to single layer electrolytes. Furthermore, multiple layers of functionally graded electrodes (anodes and/or cathodes) may be provided on single layer or composite electrolytes. [0137]
  • The textured surface(s) [0138] 203, 205 illustrated in FIGS. 13 and 15 may be textured by several different methods. In one preferred aspect of the third embodiment, the textured surface is formed by laser ablating the green sheet, following by sintering the green sheet. Any suitable laser ablation method and apparatus may be used to texture the green sheet. A schematic illustration of a laser ablation apparatus 250 suitable for texturing the green sheet surface is shown in FIG. 17. A laser source 251 directs a laser beam 253 at a reflective mirror 255. The mirror 255 directs the beam 253 through a focusing lens 257 onto the green sheet (such as an unfired electrolyte tape) 261 located on the precision XYZ table 259. Any laser source 251 which has sufficient power to ablate the green sheet 261 may be used. For example, excimer or YAG lasers may be used as the laser source 251. The laser beam 253 is scanned over the surface of the green sheet 261 by moving the XYZ table and/or by moving the mirror 255. The laser beam power may be varied during the scanning to achieve a non-uniform textured green sheet surface. For example, the laser source 251 may be periodically turned on and off, or it may be attenuated by an attenuator (not shown) to vary the laser beam power. Alternatively, the XYZ table may be moved up and down during the scanning of the beam 253 to vary- the beam power that impinges on the green sheet 261. The laser beam 253 ablates (i.e., removes or roughens) a portion of a top surface of the green sheet 261 to leave a textured surface. The textured green sheet is then sintered or fired to form the ceramic electrolyte.
  • Alternatively, the textured surface of the green sheet may be formed by photolithography methods that are used in semiconductor manufacturing. For example, as shown in FIG. 18, an [0139] etching mask 271 is formed on the green sheet 261. The etching mask 271 may comprise a photoresist layer that has been exposed through an exposure mask and developed. The unmasked portions 273 of the green sheet are etched to form recesses in the top surface of the green sheet. The masked portions 275 of the green sheet are protected from etching by the mask 271, and remain as protrusions 275 between the recesses 273. The protrusions 275 and recesses 273 form a textured surface. The photoresist mask 271 is removed after etching by a conventional selective removal process, such as ashing. Any etching gas or liquid that preferentially etches the green sheet material to the mask material may be used. As shown in FIG. 18, an anisotropic etching medium was used to form recesses 273 with straight sidewalls. This results in rectangular protrusions 275 between the recesses. Alternatively, an isotropic etching medium may be used to form recesses 273 with outwardly sloped walls. This results is trapezoidal or pyramidal protrusions 275 between the recesses.
  • The mask may comprise materials other than photoresist. In one example, other photosensitive layers may be used. Alternatively, a so-called “hard mask” may be used as a mask to etch the green sheet. For example, as shown in FIG. 19, a [0140] hard mask layer 281 is deposited on the green sheet 261. The hard mask layer 281 may be any material which resists being etched by an etching medium to a higher degree than the green sheet 261. The hard mask layer may be any suitable metal, ceramic, semiconductor or insulator. A photoresist mask 271 is formed, exposed and developed over the hard mask layer 281. The hard mask layer 281 is then etched using the photoresist as a mask. Then, the green sheet 261 is etched to form a textured surface containing a plurality of recesses 273 and protrusions 275 using the hard mask 281 as a mask. The photoresist mask 271 may be removed before or after the green sheet is etched. The hard mask 281 is removed after the green sheet 261 is textured by a selective etching medium which removes the hard mask 281 but does not etch the green sheet 261.
  • In another example, the mask may comprise a plurality of particles. As shown in FIG. 20, a plurality of discontinuous particles [0141] 291 are formed on the surface of the green sheet 261. The particles 291 may be any material which resists being etched by an etching medium to a higher degree than the green sheet 261. The particles may be any suitable metal, ceramic (such as titania or alumina), semiconductor (such as polysilicon or silicon carbide) or insulator. The particles may be formed by any particle deposition method, such as spray coating, dip coating, ink jet deposition, sputtering or chemical vapor deposition. The portions 273 of the green sheet 261 that are not covered by the particles 291 are etched to form recesses in the top surface of the green sheet. The covered portions 275 of the green sheet are protected from etching by the particles 291, and remain as protrusions between the recesses 273. The protrusions 275 and recesses 273 form a textured surface. The particles 291 are removed after the green sheet 261 is textured by a selective etching medium which removes the particles 291 but does not etch the green sheet 261.
  • Alternatively, rather than depositing the particles [0142] 291 directly on the green sheet 261, the particles 291 may be formed by etching a textured layer 293 on the green sheet 261. For example, as shown in FIG. 21, a layer 293 with a rough or textured surface is deposited on the green sheet 261. The textured surface of layer 293 contains protrusions 295. This layer 293 may be any material with has a rough surface, such as hemispherical grain polysilicon, ceramic, insulator or metal. Layer 293 is then anisotropically etched until only the protrusions 295 remain on the surface of the green sheet 261, as shown in FIG. 22. The remaining protrusions 295 appear as a plurality of particles on the green sheet 261. The green sheet 261 is then etched using the protrusions 295 as a mask.
  • In other examples, the textured surface is formed without a mask. In one example, an etching medium, such as an etching liquid, which preferentially attacks the [0143] grain boundaries 297 of the green sheet 261 is applied to an upper surface of the green sheet. The etching medium selectively etches the grain boundaries 297 of the green sheet to form recesses 273. The regions of the green sheet 261 between the grain boundaries 297 are not etched or are etched to a lesser degree and remain as protrusions 275, as shown in FIG. 23. Thus, a textured surface comprising protrusions 275 and recesses 273 is formed without a mask.
  • In another example, the textured surface is formed by embossing. A body [0144] 298 (i.e., a press, etc.) having a textured or roughened lower surface 299 is pressed into the top surface of the green sheet 261, as shown in FIG. 24. The lower surface 299 of body 298 has a higher hardness than the green sheet 261. The body 298 may be a ceramic, insulator or a metal body with a suitable hardness to emboss the green sheet. The embossing step leaves impressions or recesses in the green sheet 261 to form the textured surface in the green sheet. It should be noted that both sides of the green sheet 261 may be textured by the methods described above.
  • In another example, the textured surface is formed by building the ridges on a flat green tape. This can be done using a cladding process or by a powder/slurry spray process, where the powder and/or slurry is made of the same material as the green tape. [0145]
  • It is also possible to create the textured surface on a flat “sintered” sheet or tape as opposed to the green sheet or tape. While, in general, the green sheet or tape is more easily textured than the sintered ceramic product, etching agents that etch a sintered ceramic may be used to etch the sintered electrolyte. [0146]
  • In one aspect of this embodiment, the green tape is prepared by tape casting. In this fabrication procedure, a raw ceramic powder, for example YSZ, is mixed with solvents, binders, plastisizers, and defloculants to form a slurry. The slurry is applied to a mylar film (“carrier”) and spread uniformly with a blade, which is dragged along the length of the carrier with a precisely adjusted gap between the blade and the carrier. In large scale fabrication, this process is run continuously by moving the carrier under a static blade and applying slurry to the carrier upstream of the blade. The thickness of the green tape can range between about 20 micrometer and 10,000 micrometers, preferably about 50 to 1,000 micrometers. The amplitude of the surface texture can vary between 5 micrometers and 1000 micrometers, preferably about 10 to 30 micrometers. [0147]
  • The surface texturing can also be applied to electrolytes formed by other methods, such as electrolytes formed by extrusion. The texturing is not limited to electrolytes with planar geometries, but can also be applied to electrolytes with non-planar geometries. [0148]
  • IV. The Fourth Preferred Embodiment [0149]
  • In the fourth preferred embodiment of the present invention, the inventors have realized that the quality, robustness and environmental endurance of the solid oxide fuel cell can be improved by using an environment tolerant anode catalyst. For example, when feeding a fuel contaminated with sulfur, a solid oxide fuel cell anode catalyst that is tolerant to sulfur may be used. When the fuel cell is subject to operation in a fuel starvation mode, a fuel cell anode catalyst that is tolerant to fuel starvation may be used. [0150]
  • In the prior art low temperature acid fuel cells, some minor improvement in sulfur tolerance has been observed when certain compounds are added to the fuel side anode catalyst. The compounds that have shown some positive tolerance include MoWO[0151] x, RuO2, WOx (such as WO2.5), MOS2, WS2, and PtSx. In the prior art molten carbonate fuel cells, some minor improvement in sulfur tolerance has been observed when certain compounds are added to the fuel side anode catalyst. The compounds that have shown some positive tolerance include Cr2O3, FeO, Fe2O3, Fe3O4, Al2O3, LiAlO2, LiCrO2, MO2, MO3 and WO3, as described in U.S. Pat. No. 4,925,745, incorporated herein by reference.
  • However, the low temperature acid fuel cell is fundamentally different than the solid oxide fuel cell. In the acid fuel cell, the ionized fuel must pass through the electrolyte to be reduced at the cathode by an oxidant. The fuel ion in this case is the hydrogen proton. When sulfur is present in the fuel, the ionization reaction at the anode is slowed. The mechanism for this occurrence is not well known, but it is believed to be related to the masking of the catalyst with the sulfur adsorbed onto the active catalytic material. In contrast, in the solid oxide fuel cell, it is the oxidant oxygen anion that must pass through the electrolyte to oxidize the fuel. The sulfur contamination of the fuel creates no hindrance for the ionization of the oxygen or its transport through the electrolyte. [0152]
  • The fundamental differences between the two types of fuel cells can best be shown in FIG. 25. FIG. 25 compares the functionality of the solid [0153] oxide fuel cell 400 and an acid fuel cell 410.
  • Referring to the [0154] acid fuel cell 410, the electrolyte 411 can be a membrane such as duPont's Nafion® or an inert matrix filled with phosphoric acid. Other acids may be used, but the Nafion® and matrix phosphoric acids are the more frequently used. The cathode electrode 412 is attached to or placed against the electrolyte 411 and usually contains platinum metal as the ionization catalyst for the air oxidant 414. The platinum is often a finely divided platinum black bonded with Teflon or platinum supported on carbon and bonded with Nafion® ionomer. The anode electrode 413 is also attached to or placed against the electrolyte 411 and is similar to the cathode electrode 412, except that ruthenium, rhodium, or other metals are frequently added to the platinum to make the anode electrode 413 more tolerant to CO gas in the hydrogen fuel 415. For many fuel cell applications, the source of hydrogen fuel 415 is a reformed hydrocarbon fuel. Usually the fuel source is scrubbed of sulfur down to the parts per billion (PPB) range. Otherwise, the anode electrode 413 functionality is significantly reduced. Additionally, the reformed fuel is processed to reduce the CO volume content in the hydrogen fuel 415 to less than 50 parts per million (PPM) to minimize the poisoning effect on the electrode. The hydrogen fuel 415 is ionized at anode electrode 413 producing hydrogen protons. The protons then pass through the membrane 411 by the gradient created by the combination with oxygen anions produced on the cathode electrode 412 from air oxidant 414 to produce product water 412.
  • Referring to solid [0155] oxide fuel cell 400, the electrolyte 401 is preferably yttria-stabilized zirconia (YSZ), although other ceramic oxides, such as ceria are sometimes used together with or instead of YSZ. A preferred cathode electrode 402 is made from a 50:50 mixture of YSZ and La0.8Sr0.2MnO3 (LSM). Other materials may be used if desired. The cathode electrode 402 is attached to or placed against the electrolyte 401 and ionizes the oxygen in the air oxidant 404. The oxygen anions pass through the electrolyte 401 by the gradient created by the consumption of the anions by combination with fuel ions. In the prior art solid oxide fuel cells, the anode electrode 403 is a often a ceramic-metallic (cermet) of Ni and YSZ, while Cu is sometimes used instead of Ni. Hydrogen fuel 405 is ionized at the anode electrode 403 and combines with the oxygen anions to form water.
  • One of the significant advantages of the solid oxide fuel cell is the potential for direct hydrocarbon fuel feed to the operating cell anode. The prior art Ni/YSZ anode electrode performs very well with pure hydrogen fuel, but when attempting to internally reform a hydrocarbon fuel into a hydrogen rich fuel stream the Ni/YSZ anode electrode has shortcomings related to carbon formation and sulfur poisoning. To reduce carbon formation in the prior art solid oxide fuel cell, water (i.e., water vapor) is added to the hydrocarbon fuel to prevent carbon formation. Although the fuel cell product water is generated within the anode electrode, even more water must be added to the fuel to prevent the carbon formation. This extra water must be introduced with the incoming fuel, which complicates the operation of the fuel cell. Second, the prior art Ni/YSZ electrode cannot tolerate even the 10 ppm sulfur normally found in natural gas. Thus, expensive sulfur scrubbing equipment is often used to reduce the sulfur content of the fuel, which increases the cost of the electricity generation. [0156]
  • Thus, in a first preferred aspect of the fourth embodiment, sulfur tolerant compounds are used in combination with or instead of Ni in the anode cermet of a solid oxide fuel cell. The sulfur tolerant compounds include any compounds which increase the anode tolerance to sulfur in the fuel stream. While the inventors do not want to be bound by any theory of operation of the sulfur tolerant compounds, it is believed that the sulfur tolerant compounds prevent or reduce the formation of sulfur on the anode. The preferred sulfur tolerant compounds include MoWO[0157] x, RuO2, WOx, such as WO2.5, MOS2, WS2, and PtSx. Some compounds, such as WOx are also CO tolerant. Less preferred compounds include sulfur tolerant catalysts usable in a molten carbonate fuel cell, such as Cr2O3, FeO, Fe2O3, Fe3O4, Al2O3, LiAlO2, LiCrO2, MO2, MO3 and WO3, as described in U.S. Pat. No. 4,925,745, incorporated herein by reference. Preferably, the anode cermet comprises the ceramic, such as (YSZ), and a catalyst. The catalyst preferably comprises 10 to 90 weight % Ni or Cu and 10 to 90 weight percent of the sulfur tolerant compound. Most preferably, the catalyst comprises 30 to 70 weight % Ni or Cu and 30 to 70 weight percent of the sulfur tolerant compound. However, some sulfur tolerant compounds, such as PtSx, may be used without Ni or Cu and comprise 100% of the catalyst.
  • These sulfur tolerant catalyst compounds in combination with or replacing the Ni in the anode electrode cermet provide an increased tolerance to sulfur in the fuel. The sulfur tolerant catalyst allows the solid oxide fuel cell to be used with a hydrogen fuel source containing contaminate levels of sulfur compounds, such as more than 10 ppb, for example more than 100 ppb. The three elements that combine in a non-obvious manner to achieve this tolerance include: weak tolerance of the Ni cermet to sulfur, uninhibited availability of an oxidant within the anode electrode, and elevated operational temperature. [0158]
  • In another preferred aspect of the fourth embodiment, the environmental tolerant anode catalyst comprises a fuel starvation tolerant catalyst. When the solid oxide fuel cell is operating at steady state, the reactants are independently flow controlled. The cathode airflow is generally controlled to supply sufficient oxygen for the cathode reaction and to remove the waste heat from the fuel cell reaction. Usually airflow 1.5 to 2.5 times the stoichiometric requirements is ample to satisfy the cathode reaction. Heat removal will generally require much more airflow than that required in satisfying the cathode reaction and therefore, there is no reasonable concern that a cell will become oxygen starved. [0159]
  • On the other hand, the fuel is flow controlled only to support the anode reaction. In this case, the fuel flow is generally set at about 1.2 times the stoichiometric requirements of the anode in order to maintain a high level of fuel utilization. This high level of fuel utilization is required to obtain a high overall system efficiency. [0160]
  • In the prior art solid oxide fuel cells, a problem develops when there is an instantaneous requirement for an increased electrical output from the solid oxide fuel cell stack. Under these conditions, the air supply is more than ample to support the increased reaction rates within all the cells. However, one or more cells in the stack can be fuel starved until the fuel control adjusts the fuel flow to the new reaction rates. During the few seconds that it takes to adjust the fuel flow, the anode catalyst can be permanently damaged. Since the cells in a planar solid oxide stack are in electrical series, the entire stack can be rendered useless. [0161]
  • The fundamental reason for cell anode damage is illustrated in FIG. 26. FIG. 26 shows the functionality of the solid [0162] oxide fuel cell 500 in the normal anode and normal cathode reaction modes and the anode reaction in the fuel starved mode.
  • Referring to the solid [0163] oxide fuel cell 500 in the normal operating mode, the electrolyte 501 is usually yttria-stabilized zirconia (YSZ), although other ceramic oxides such as ceria are sometimes used. The typical cathode electrode 502 is made from a 50:50 mixture of YSZ and La0.8Sr0.2MnO3 (LSM). Other materials may be used if desired. The cathode electrode 502 is attached to or placed against the electrolyte 501 and ionizes the oxygen in the air oxidant 504. The oxygen anions pass through the electrolyte 501 by the gradient created by the consumption of the anions by combination with fuel ions. A prior art anode electrode 503 is configured with a ceramic-metallic (cermet) of Ni and YSZ. Alternately, Cu is sometimes used as the metal in the cermet for the anode electrode. Hydrogen/CO fuel 505 is ionized at the anode electrode 503 and combines with the oxygen anions to form water and CO2.
  • When a section of an individual solid oxide fuel cell within a stack becomes fuel starved, the cell becomes an electrical load instead of an electrical power generator. This occurs because other cells in the stack have sufficient fuel to support the reaction and these cells drive the cell(s) that has become a load. Under these conditions, the fuel starved cell polarity reverses and oxygen is evolved from the anode. The cathode electrode and the electrolyte continue to operate as they had when operation in the fuel cell mode. [0164]
  • When the fuel flow rate is restored to normal, the load cell(s) reverts back to the power generating fuel cell mode. Unfortunately, in the process of evolving oxygen, the standard Ni/YSZ anode electrode is oxidized and permanently damaged because Ni is not a fuel starvation tolerant catalyst. [0165]
  • The present inventors have realized that if a metal which forms a reversible oxide without damage to the metal is added to the anode, then the anode is rendered fuel starvation tolerant. Such a metal forms an oxide when oxidized and reverts back to a pure metal without significant damage when the oxide is reduced by the fuel reaction at the anode. Preferably, the fuel starvation tolerant compound include platinum group metals, such as platinum, palladium, rhodium, iridium, osmium and ruthenium. Low temperature water electrolysis shows that platinum metal electrodes can be oxidized and reduced without damage. Other catalytic materials or additives that display this characteristic include ruthenium and tungsten at various oxide levels. The use of these metals/oxides in various ratios provides the tolerance to the oxidative anode conditions during fuel starvation. [0166]
  • Preferably, the [0167] anode 503 comprises a cermet which includes the ceramic, such as (YSZ), and a fuel starvation tolerant catalyst. The catalyst preferably comprises 10 to 90 weight % Ni or Cu and 10 to 90 weight percent of the fuel starvation tolerant material. Most preferably, the catalyst comprises 30 to 70 weight % Ni or Cu and 30 to 70 weight percent of the fuel starvation tolerant material. Preferably, the fuel starvation tolerant material oxidizes preferentially to Ni during fuel starvation. However, some fuel starvation tolerant materials, such as Pt, may be used without Ni or Cu and comprise 100% of the catalyst.
  • In a third preferred aspect of the fourth embodiment, the anode comprises an environmental tolerant catalyst which is both a sulfur tolerant catalyst and a fuel starvation tolerant catalyst. For example, the anode may contain a combination of similarly based fuel starvation and sulfur tolerant materials, such as Pt and PtS[0168] x, Ru and RuO2, and W and WOx. Alternatively, the anode may contain a combination of dissimilar catalysts, such as a Pt—WOx or Pt—HXWO3 as disclosed in U.S. Pat. No. 5,922,488 incorporated herein by reference in its entirety. Thus, any combination of the sulfur tolerant and fuel starvation tolerant materials described above may be selected for the anode composition.
  • Preferably, the [0169] anode 503 comprises a cermet which includes the ceramic, such as (YSZ), and a environment tolerant catalyst. The catalyst preferably comprises 10 to 90 weight % Ni or Cu, 5 to 45 weight percent of the sulfur tolerant material and 5 to 45 weight percent of the fuel starvation tolerant material. Most preferably, the catalyst comprises 30 to 70 weight % Ni or Cu, 15 to 35 weight percent of the sulfur tolerant material and 15 to 35 weight percent of the fuel starvation tolerant material. However, some sulfur tolerant and fuel starvation tolerant materials, such as Pt, may be used without Ni or Cu and comprise 100% of the catalyst.
  • The anodes may be formed using any known cermet fabrication methods. The Ni or Cu metals, sulfur tolerant materials and/or the fuel starvation tolerant materials may be incorporated into the cermet by any suitable method. For example, these materials may be deposited by co-deposition, co-electrodepositon, freeze drying or sequential deposition. Thus, the environmental tolerant material may be alloyed or admixed with Ni or Cu and then provided into the YSZ to form the cermet. For example, the environmental tolerant material may be alloyed or admixed with Ni or Cu and then provided into YSZ using a wet (solution), a dry (powder) or a sputtering process. Alternatively, the environmental tolerant material may be alloyed or admixed with Ni or Cu and then placed on a support, such as a foam support or a dry ice support, and then pressed into contact with the YSZ. The catalyst is diffused into the YSZ to form the cermet by sintering and/or pressing. If dry ice is used, then the dry ice is sublimed to diffuse the catalyst into the YSZ. [0170]
  • V. The Fifth Preferred Embodiment [0171]
  • In the fifth embodiment of the present invention, the inventor has realized that the solid oxide fuel cell system can be simplified, when feeding a hydrocarbon fuel directly to the solid oxide fuel cell anode for internal reforming to a hydrogen rich reactant by supplying the reforming process steam from the anode exhaust enthalpy recovery. In other words, only the product water (i.e., water vapor) is added to the fuel provided into the anode. [0172]
  • In the low temperature PEM fuel cells, cathode enthalpy is recovered and returned to the cathode inlet to prevent the dry out of the water saturated membrane. In this case, the incoming oxidant air is humidified and membrane dry out is avoided. Several methods have been developed to accomplish this water and heat transfer including hydrated membranes, water injection, and cycling desiccants. One method includes using a device called an enthalpy wheel. The enthalpy wheel is a porous cylindrical wheel with internal passages that are coated with desiccant. It rotates slowly in one direction, allowing the transfer of sensible and latent heat from the hot saturated air exhaust to the cool dry air inlet. [0173]
  • In the solid oxide fuel cell, there is no need to maintain the saturation of any of the components. In the case of a solid oxide fuel cell operating with pure hydrogen and air reactants, these reactants can be absolutely free of any water vapor. The prior art Ni/YSZ anode electrode performs very well with pure hydrogen fuel. However, when attempting to internally reform a hydrocarbon fuel into a hydrogen rich fuel stream, the Ni/YSZ anode electrode has shortcomings related to carbon formation. To reduce carbon formation in the prior art solid oxide fuel cell, water (i.e., water vapor) is added from an external boiler to the hydrocarbon fuel to prevent carbon formation on the anode. For the purpose of fuel steam reforming within the anode of a solid oxide fuel cell, a high rate of water vapor (i.e., steam), amounting to approximately a 3:1 steam to carbon ratio, must be injected into the fuel before introduction into the fuel cell anode. The use of the extra boiler complicates the electricity generation process and increases its cost. [0174]
  • The present inventors realized that product water vapor emitted from the anode side exhaust of the solid oxide fuel cell may be recirculated into the fuel being provided into the anode input to prevent or reduce the carbon formation on the anode. The enthalpy wheel is a preferred device to control the water and heat transferred from the anode exhaust of a solid oxide fuel cell to the anode inlet. The control of the amount of water introduced with the fuel is used to prevent carbon formation with too little water and to prevent fuel starvation with too much water. The water transfer rate is controlled by the speed of the wheel. [0175]
  • The fundamentals of the [0176] system 600 employing an enthalpy wheel in the solid oxide fuel cell fuel stream are illustrated in FIG. 27A. The hydrocarbon fuel supply is delivered through conduit 604 to enthalpy wheel 601. Within the enthalpy wheel 601, the fuel supply receives water vapor and heat from the anode side fuel exhaust. The warm wet fuel supply is then delivered-to an optional heat exchanger 602 through conduit 605. Within the heat exchanger 602, the fuel exhaust heats the warm wet fuel supply further. The hot wet fuel supply is then delivered to the anode chambers within the solid oxide fuel cell stack 603 through conduit 606. Within the solid oxide fuel cell anode chambers the hot wet hydrocarbon fuel supply is reformed into a mixture of hydrogen, water vapor, and carbon oxides. Nearly simultaneously, most of the hydrogen and carbon monoxide are converted to more water vapor and more carbon dioxide, respectively, from the reaction with the oxygen anions in the anode catalyst.
  • The fuel exhaust gasses, with significantly more water vapor than was introduced into the solid oxide fuel cell anode chambers, return to [0177] heat exchanger 602 through conduit 607. Within heat exchanger 602 some of the heat in the exhaust stream is given up to the inlet fuel supply. The fuel exhaust is then delivered back to the enthalpy wheel 601 through conduit 608. Within the enthalpy wheel 601, much of the water vapor and remaining heat in the fuel exhaust is transferred to the inlet fuel supply.
  • The-rotational speed of the enthalpy wheel is modulated to optimize the water vapor flux. The fuel exhaust then leaves the system through [0178] outlet conduit 609. Preferably, 0% to 90%, such as 20 to 70% of the product water vapor is transferred to the fuel supply. Preferably, all heat transferred to the fuel supply is through the enthalpy wheel and heat exchanger.
  • In an alternative embodiment, the enthalpy wheel is replaced with at least two adsorption beds, as illustrated in FIG. 27B. The [0179] first adsorption bed 610 is used to adsorb water and water vapor from the anode exhaust, while letting anode exhaust gases, such as CO, CO2, H2 and methane, to pass through to the outlet conduit 609. The second adsorption bed 611 is used to provide water that was previously collected from the anode exhaust. When the supply of water is exhausted in the second bed 611, the anode exhaust is provided into the second bed, while the first bed 610 is used to provide the water or water vapor into the inlet fuel. If desired, a reformer may also be added between the fuel inlet 604 and the fuel cell stack 603, preferably between the heat exchanger 602 and the fuel cell stack 603.
  • Any suitable method may be used to provide anode exhaust and fuel supply through the adsorbent beds. For example, as shown in FIG. 27B, a [0180] first valve 612, such as a four way valve, switches fuel input from fuel inlet 604 between the first 610 and the second 611 adsorbent bed. The valve 612 also switches the exhaust being provided from the first 610 or the second 611 beds to the outlet conduit 609. The conduit 608 connects the first adsorbent bed 610 with a first heat exchanger inlet 614 or a first heat exchanger outlet 615 via a second valve 613, such as a four way valve. The conduit 605 connects the second adsorbent bed 611 with the first heat exchanger inlet 614 or the first heat exchanger outlet 615 via valve 613. When the valve 613 is in a first position, it provides a fluid path between the first adsorbent bed 610 and the first heat exchanger outlet 615 and between the second adsorbent bed 611 and the first heat exchanger inlet 614. When the valve 613 is in a second position, it provides a fluid path between the first adsorbent bed 610 and the first heat exchanger inlet 614 and between the second adsorbent bed 611 and the first heat exchanger outlet 615. If desired, other configurations may be used. For example, four way valve 613 may be replaced with two three way valves, each respective valve being located between the heat exchanger 602 and respective conduits 605, 608.
  • During operation, the [0181] system 600 can be run without using a boiler to provide water vapor into the inlet fuel. However, a small boiler may be added to the system. This boiler may be run during operation start up to provide water into the fuel inlet while the system is warming up and sufficient water vapor is being generated at the anode exhaust.
  • This system is advantageous because it provides simple transfer of water vapor and heat in a controlled fashion such that the proper conditions at the solid oxide fuel cell anode electrodes for internal steam reforming are met. The enthalpy wheel and heat exchanger may be used to provide the entire supply of water vapor and heat for the fuel supply to operate the solid oxide fuel cell. [0182]
  • VI. The Sixth Preferred Embodiment [0183]
  • The sixth preferred embodiment is directed to a felt seal. Fuel cell stacks, particularly those with planar geometry, often use seals between electrolyte and interconnect surfaces to contain fuel and air (see FIG. 28). These seals must maintain their integrity at high operating temperatures and (on the cathode side) in an oxidizing environment. Furthermore, expansion and contraction of the seal and the components in contact with the seal due to thermal cycling or compression should not result in damage of any of the components during its expected life. [0184]
  • Many compliant seals, such as elastomeric o-rings and gaskets, do not crack and tend to absorb stresses in an assembly that arise from thermal expansion and compression. However, these seals cannot be used at high temperatures because the elastomeric materials used in them decompose, degrade, or oxidize. [0185]
  • Many types of seals used at elevated temperatures, such as brazes and metal gaskets, are not compliant or elastic. Some assemblies are difficult to seal with brazes or gaskets because of operating conditions or material incompatibilities. They may often have a limited life as well, tolerating only a relatively few number of thermal cycles before they fail. Also, when some assemblies are sealed with these materials, differences in the coefficients of thermal expansion result in mechanical stresses that can lead to failure of the seal or the components of the assembly. Also, non-compliant seals often present difficulties and high costs of fabrication and assembly due to the tighter tolerances which are required, in flatness for example. [0186]
  • The sixth preferred embodiment is directed to a sealing arrangement that is both compliant and capable of operating at high temperatures in oxidizing and reducing environments. The sealing member is capable of sealing dissimilar materials, such as a metal and a ceramic, and similar materials that may or may not differ in composition, such as two ceramics or two metals. Since the sealing member is elastic and compliant at device operating temperatures, it may be used to seal two materials with dissimilar coefficients of thermal expansion. This seal may be advantageously used in a solid oxide fuel cell, where the operating temperatures are in the range of 600 to 800° C. [0187]
  • A gas-tight compliant seal between surfaces can be made from a felt. Here, “felt” is used to describe a compliant layer of a material that can endure the elevated operating temperature and atmosphere of the device it is being applied to. In some cases, the felt may be composed of a malleable metal or alloy. However, this definition does not restrict this term to metals. The compliant layer can for example be made from non-metallic fibrous materials, such as silica. This compliant layer can be made up from fibers, as indicated by the word “felt,” but also other thick and compliant constructions, for example foams, such as small cell foams. Thus, the seal is preferably made from a compliant metal or a ceramic fibrous or foam material. [0188]
  • The felt is made gas impermeable by one of several means, and is sealed by one of several means to the mating surfaces. The felt gives compliance to the seal, allowing it to absorb stresses caused by compression and thermal expansion and contraction of the assembly of which it is part. The means used to make the felt impermeable and to seal the felt to the mating surfaces are also compliant in nature. Appropriate selection of the composition of the various elements of the seal allows the seal to be made according to various criteria, including operating temperatures, oxidizing or reducing environments, and cost. [0189]
  • Two mating surfaces ([0190] 701 and 702) are shown in FIG. 28. A seal must be made between these two surfaces in order to prevent gas exchange in either direction between sides 705 and 706.
  • In one case shown in FIG. 28, a [0191] felt sealing member 710 is placed between the mating surfaces 701 and 702. The felt sealing member 710 is sealed to the mating surfaces through application of a sealing material 720 that is soft at the device operating temperature but is impermeable to the gases of interest in the application. For example, this may be a glass or glaze compound. One example of a glaze is a Duncan® ceramic glaze GL611. This material can be applied to the felt or to the mating surfaces prior to assembly, for example by dipping the felt sealing member and/or the mating surfaces into the molten glass or glaze. The material softens at elevated temperatures and mates the felt to the surfaces, but remains impermeable to gases. The material 720 is optional if the felt seal contains appropriate means of mating the felt to the surfaces, as is the case in many preferred aspects.
  • The felt sealing [0192] member 710 is made impermeable to gases by one of several ways. In one preferred aspect, the porous felt is filled prior to assembly with a filler material 730 that is soft at the device operating temperature. For example, this may be a glass or glaze mixture. After firing, the glassy residue makes the felt impermeable to gases, but because the material 730 softens at the operating temperature, the felt-glass composite remains compliant. In subsequent paragraphs and figures, it is assumed that same-numbered items carry their previous definitions.
  • In another preferred aspect (FIG. 29), the felt sealing [0193] member 710 is made impermeable to gases by melting a felt surface 740 into a solid layer that is non-parallel, such as perpendicular, to the mating surfaces. The solid layer which is formed to be thin enough to remain flexible. A solid layer means a layer that has a much lower porosity than the felt, such as a porosity of 70% or less than the felt. This solid layer may be formed by selectively heating a portion of the felt sealing member 710 to transform the heated portion to a solid layer, such as a closed cell metal foam layer. For example, a surface 740 of the felt sealing member 710 may be selectively heated by a laser to form the solid layer.
  • In another preferred aspect (FIG. 30), the felt sealing [0194] member 710 is made impermeable to gases by forming a solid layer 750 on felt sealing member 710 that is perpendicular and parallel to the mating surfaces described previously. The parallel solid surfaces provide an improved contact area for the seal.
  • In another preferred aspect (FIG. 31), the felt sealing [0195] member 710 is made impermeable to gases through application of a barrier foil layer 760 that is non-parallel, such as perpendicular, to the mating surfaces. The foil adheres to the felt via a material such as that which is used to attach the felt to the mating surfaces. Alternatively, the foil may be pressed into place and held by a second felt sealing member or other component. The foil 760 is compliant because it is thin. Preferably, the foil is a thin metal foil. The foil extends between mating surfaces 701, 702 to block the flow of gas between sides 705 and 706.
  • In another preferred aspect (FIG. 32), the felt sealing [0196] member 710 is made impermeable to gases through application of several foils. Foil 770 is non-parallel, such as perpendicular, to the mating surfaces as described previously, and foils 772 and 774 extend into the area parallel to the mating surfaces. These foils 772, 774 provide improved contact area for the sealing member. They may also produce adhesion between the sealing member and the mating surfaces. The foils 770, 772, and 774 may be the same or different materials depending on the various compositions of the felt 710 and mating surfaces 701 and 702. They may comprise separate components or one continuous piece of foil.
  • In another preferred aspect (FIG. 33), the felt sealing [0197] member 710 is made impermeable to gases through deposition of a gas impermeable material layer on the felt 710. This material may be deposited on the felt by various methods, including but not restricted to, dipping and evaporation, physical vapor deposition, chemical vapor deposition, thermal spray, plasma spray, and precipitation from a liquid. Material portion 780 is non-parallel, such as perpendicular, to the mating surfaces 701, 702. Preferably, portions 782, 784 of the gas impermeable material layer extend into the area parallel to the mating surfaces 701, 702. These portions 782, 784 provide an improved contact area for the sealing member. They may also produce adhesion between the felt sealing member 710 and the mating surfaces. The impermeable material layer portions 780, 782, and 784 may be the same or different materials depending on the various compositions of the felt 710 and mating surfaces 701 and 702.
  • In another preferred aspect (FIG. 34), the felt sealing [0198] member 790 is made impermeable to gases in its initial preparation. For example, the felt may be prepared as a closed-cell foam.
  • The felt composition can be selected so as to operate well in the atmosphere present in the device containing the felt seal. For example, in an oxidizing atmosphere the felt may be composed of a suitable M—Cr—Al—Y material, where M comprises at least one metal selected from Fe, Co, or Ni. In another example, the felt may be composed of Inconel alloy. In another example, in a reducing atmosphere, the felt may be composed of nickel. Other metals, alloys, or indeed other malleable materials or compounds metal may be used depending on the application requirements. One example of forming a felt sealing member [0199] 710 (nickel felt) with a gas impermeable material 730 (glass) is as follows. A nickel felt (i.e. foam) with a density of 15% relative to solid nickel is saturated with a molten glass. The felt is fired to remove volatiles, leaving behind a glass residue that renders the felt impermeable to gases. The felt is placed between two mating surfaces, for example a metal sheet and zirconia. To each of the mating surfaces a layer of glass seal is applied where the felt-glass composite will contact the surfaces. The felt is placed between the surfaces, compressed, and fired.
  • The seal can take the shape of the mating surfaces to be sealed. For example, if the mating surfaces are rectangular, the seal may take the form of a rectangular gasket. If the mating surfaces contain open areas, such as in an assembly with internal gas manifolds or flow ducts, the seal can accommodate and seal such open areas. This is illustrated in FIG. 35, where one of the mating surfaces ([0200] 794) contains flow channels which are sealed from the center of the surface and from the exterior of the surface by the felt gasket 797.
  • All embodiments of the felt seal can be placed in a structure in one or both mating surfaces, for example in a groove in a mating surface, that provides containment and additional compression and adhesion surfaces. [0201]
  • The felt part of the seal may also serve other roles, such as current collector/distributor, flow distributor, etc. in a fuel cell stack, such as a solid oxide fuel stack. [0202]
  • VII. The Seventh Preferred Embodiment [0203]
  • The seventh preferred embodiment is directed to felt current conductors/gas flow distributors for fuel cell stacks. Fuel cell stacks, particularly those with planar geometry, often use utilize some material to conduct electrons from the anode to the separator plate and from the separator plate to the cathode. This material typically has a better electrical conductivity than the porous electrode (i.e., anode and/or cathode) material. Usually this material is distinguished from the electrodes in that it also must provide flow distribution of oxygen- or fuel-bearing gases. This material is often called a current conductor/gas flow distributor (“conductor/distributor” herein after). In some cases, these conductor/distributors may provide structural support to the fuel cell stack. Some examples of prior art conductor/distributors include metal wire coils, wire grids, and metal ribs. These may be used independently or in some combination. [0204]
  • The prior art conductor/distributors sometimes exhibit less-than-optimal current conduction or gas flow distribution properties. They are also costly to implement. Also, many of the prior art conductor/distributors are not compliant (i.e., not elastic at the fuel cell operating temperatures). Non-compliant components often present difficulties and high costs in fabrication and assembly of the fuel cells due to the tighter fuel cell tolerances which are required. [0205]
  • The present inventors realized that a porous conductive felt can serve as a current conductor and gas flow distributor with better properties than the prior art conductor/distributors and may be less costly to implement. In some preferred aspects, the felt conductor/distributor can also serve as a seal or as a support for other fuel cell stack components. The use of a compliant, conductive felt reduces the probability of component and assembly failure during thermal cycling and compression of a fuel cell stack, preferably a high temperature fuel cell stack, such as a solid oxide or molten carbonate fuel cell stack. [0206]
  • Here, “conductive felt” is used to describe a compliant layer of electrically conductive material that can endure the operating temperature and atmosphere of the device (i.e., fuel cell stack) in which it is located. In some cases, the felt may be composed of a malleable metal or alloy. However, this definition does not restrict the term “felt” to metals. The felt conductor/distributor can for example be made from other porous, conductive materials, such as a silica-metal composite. The felt conductor/distributor should be made conductive and gas permeable and can be made up from fibers, foams and other relatively thick, compliant, conductive and gas permeable structures. [0207]
  • A conductor/distributor comprising a gas permeable (i.e., porous) conductive felt with composition chosen to be appropriate for the conditions specified by the application. For example, the felt material is chosen such that it remains conductive and gas permeable at the fuel cell operating temperature. The felt conductor/distributor is located in contact with the active area of the fuel electrode (i.e., anode or cathode). The fuel cell separator plate is placed in contact with the conductor/distributor. Various ways may be used to ensure electrical contact between electrode, conductor/distributor, and separator plate. [0208]
  • FIG. 36 shows repeating elements of a fuel cell stack containing an [0209] electrolyte 810, an anode 820, a cathode 830, anode seal 840, cathode seal 845, and a separator plate 850, such as metal plates. A second separator plate 850 is also shown in the diagram to illustrate the connection to the next cell of the stack. The stack may be internally or externally manifolded, as will be described in more detail below.
  • The [0210] anode 820 and cathode 830 are often optimized for the electrochemical reactions they are catalyzing. Often, they are not optimized for electrical conductivity or for distribution of fuel- and oxygen-bearing gases. Therefore, anode conductor/distributors 860 and cathode conductor/distributors 870 are provided to fill these roles. The separator plates 850 may be omitted if the felt conductor/distributors are constructed to also perform the function of the separator plates.
  • In one preferred aspect of the seventh preferred embodiment, the anode conductor/[0211] distributor 860 is composed of a conductive felt. The felt conducts electrons from the anode to the separator plate. Since the felt is gas permeable, it also allows fuel to reach the anode surface, and the reaction byproducts to leave the surface and exhaust from the cell. The electrical contact between anode and felt, and between separator plate and felt, may be enhanced by adding a layer of an optional adhesive or contact material. The composition of the felt is chosen as appropriate for the fuel cell operating conditions. For example, a nickel felt with a density of 15 to 35%, preferably about 25% relative to the density of solid nickel and a thickness of 0.5 to 4 mm, preferably about 2 mm may be used in a high temperature fuel cell, such as a solid oxide fuel cell, with a reducing atmosphere and a temperature of 600 to 850° C., such as 800° C. The felt may be potted in a nickel-YSZ cermet on either the anode or separator plate sides of the connection, or on both sides.
  • In another preferred aspect of the seventh preferred embodiment, the cathode conductor/[0212] distributor 870 is composed of a conductive felt. The felt conducts electrons from the separator plate to the cathode. It also allows oxygen to reach the cathode surface, and the oxygen depleted air to leave the surface and exhaust from the cell. The electrical contact between cathode and felt, and between separator plate and felt, may be enhanced by adding a layer of an optional adhesive or contact material. The composition of the felt is chosen as appropriate for the fuel cell operating conditions. For example, a Fe—Cr—Al—Y felt with a density of 5 to 30%, preferably about 15% relative to the density of the solid metal alloy and a thickness of 0.5 to 4 mm, preferably 2 mm, may be used in a high temperature fuel cell, such as a solid oxide fuel cell, in an oxidizing atmosphere at 650 to 850° C., such as about 800° C. If desired, some or all of Fe may be substituted by Co and/or Ni in the Fe—Cr—Al—Y felt. The felt may be potted in a lanthanum-strontium manganite (LSM) perovskite on either the cathode or separator plate sides of the connection, or on both sides.
  • Preferably, both the [0213] anode 860 and cathode 870 conductor/distributors are made from a felt. In subsequent paragraphs and figures, it is assumed that same-numbered items carry their previous definitions.
  • In another preferred aspect of the seventh preferred embodiment, the anode and/or cathode conductor/distributors contain a non-uniform surface. Preferably, the conductor/distributor(s) contain ribs which provide a desired pressure drop or flow distribution pattern. Other surface features, such as dimples, lines, or a particular pore geometry may be used to exercise control over pressure drop or flow distribution. [0214]
  • In another preferred aspect of the seventh embodiment (FIG. 37), the anode conductor/[0215] distributor 860 is combined with the anode-side felt seal of the sixth preferred embodiment. The anode conductor/distributor and seal is made of one continuous piece of material. The anode conductor/distributor 860 can be used in conjunction with any of the various preferred aspects of the sixth embodiment describing the felt seal.
  • In another preferred aspect of the seventh embodiment (FIG. 38), the cathode conductor/[0216] distributor 870 is combined with the cathode-side felt seal of the sixth preferred embodiment. The cathode conductor/distributor and seal is made of one continuous piece of material. The cathode conductor/distributor 870 can be used in conjunction with any of the various preferred aspects of the sixth embodiment describing the felt seal. Most preferably, both the anode and cathode conductor/distributors are combined with the felt seal.
  • In another preferred aspect of the seventh preferred embodiment (FIG. 39), the anode conductor/[0217] distributor 860 provides the structural support for the separator plate 850. In this aspect, the separator plate material may be made as thin as practicality and serviceability allows. Preferably, the separator plate comprises a thin film deposited onto the anode conductor/distributor 860 by various thin film deposition techniques, including but not limited to thermal or plasma spray, chemical or physical vapor deposition (i.e., CVD or sputtering), precipitation, and dipping. Alternatively, the thin separator plate 850 may comprise an integral component that is placed in contact with the conductor/distributor. Preferably, a “thin film” is less than 500 microns thick, more preferably, less than 100 microns thick, most preferably 10 to 30 microns thick. In this case, the felt conductor/distributor thickness is sufficient to act as a substrate for the thin film, such as a thickness of greater than 30 microns, preferably greater than 100 microns.
  • In another preferred aspect of the seventh preferred embodiment (FIG. 40), the cathode conductor/[0218] distributor 870 provides the structural support for the separator plate 850. In this aspect, the separator plate material may be made as thin as practicality and serviceability allows. Preferably, the separator plate comprises a thin film deposited onto the cathode conductor/distributor 870 by various thin film deposition techniques, including but not limited to thermal or plasma spray, chemical or physical vapor deposition (i.e., CVD or sputtering), precipitation, and dipping. Alternatively, the thin separator plate 850 may comprise an integral component that is placed in contact with the conductor/distributor. Preferably both the anode and cathode conductor/distributors serve as a support for their respective separator plates.
  • In another preferred aspect shown in FIG. 41, the anode conductor/[0219] distributor 860 serves as a seal and as separator plate support. In the figure, the anode conductor/distributor renumbered 865 is shown in one of its various preferred configurations.
  • In another preferred aspect shown in FIG. 42, the cathode conductor/[0220] distributor 870 serves also as seal and as separator plate support. In the figure, the cathode conductor/distributor renumbered 875 is shown in one of its various preferred configurations.
  • In subsequent paragraphs and figures, the conductor/distributors are described in their roles as support structures for other elements of the fuel cell stack. In these paragraphs and figures, [0221] item 865 refers to the anode conductor/distributor in one of its various previously described configurations, and item 875 refers to the cathode conductor/distributor in one of its various previously described configurations.
  • In another preferred aspect shown in FIG. 43, the anode conductor/[0222] distributor 865 and the cathode conductor/distributor 875 together support a common separator plate 850 that is located between them. The separator plate 850 may be placed or deposited in any way so as to reduce the materials and assembly costs and increase the performance and quality of the assembly. Typically the separator plate 850 would be made as thin as practicality and serviceability allows, such as a thin film plate.
  • If the felt conductor/[0223] distributors 865 and 875 are combined with the seals, then the seal portions of the conductor/distributors can be made gas impermeable by any of the methods described in the sixth preferred embodiment. Alternatively, portions of the separator plate 850 may be used to form a seal. For example, thin separator plate material or foil can be extended around the edges of either or both conductor/distributors as shown in FIG. 44. These separator plate extension act as a gas impermeable seal.
  • In another preferred aspect of the seventh embodiment shown in FIG. 45, the anode conductor/[0224] distributor 865 and the cathode conductor/distributor 875 together support not only the separator plate 850, but they also support the cathode 830, electrolyte. 810, and anode 820. The separator plate 850, cathode 830, electrolyte 810, and anode 820 may be placed or deposited in any way so as to reduce the materials and assembly costs and increase the performance and quality of the assembly. Typically these components would be made as thin as practicality and serviceability allows. These components preferably comprise thin films (as defined above) that are preferably deposited on the conductor/distributor 865/875 “substrate” by various thin film deposition techniques described above.
  • FIG. 46 illustrates a three dimensional view of an internally manifolded fuel cell stack containing a common felt conductor/distributor and seal. In FIG. 46, the fuel cell stack contains a [0225] separator plate 850, an anode felt conductor/distributor/seal 860, an electrolyte 810, and anode 820 and a cathode felt conductor/distributor/seal 870. The cathode is not visible in FIG. 46 because it is located “behind” the electrolyte 820. The separator plate 850 and electrolyte 810 contain gas passages or openings 876, 877, 878 and 879. Specifically, passages 876 are fuel inlet passages, passages 877 are fuel outlet passages, passages 878 are oxidizer inlet passages and passages 879 are oxidizer outlet passages.
  • The anode felt conductor/distributor/[0226] seal 860 is made of a conductive felt. The entire anode felt conductor/distributor/seal 860 is gas permeable, except for gas impermeable seal region or strip 880. The cathode felt conductor/distributor/seal 870 is made of a conductive felt. The entire cathode felt conductor/distributor/seal 870 is gas permeable, except for gas impermeable seal region or strip 881.
  • In the anode felt conductor/distributor/[0227] seal 860, the gas impermeable strip 880 circumscribes a gas permeable region 882 and seals it from a gas permeable region 883. In the cathode felt conductor/distributor/seal 870, the gas impermeable strip 881 circumscribes a gas permeable region 884 and seals it from a gas permeable region 885.
  • [0228] Region 882 lines up with the anode 820 and with the fuel passages 876 and 877 when the stack is assembled. Region 883 lines up with the oxidizer passages 878 and 879. Region 884 lines up with the cathode (not shown) and with the oxidizer passages 878 and 879. Region 885 lines up with fuel passages 876 and 877.
  • The fuel cell stack operates as follows. The input or inlet fuel [0229] 886 (dashed lines in FIG. 46) is provided into fuel inlet passage 876 in separator plate 850. The fuel reaches the gas permeable region 882 in the anode conductor/distributor/seal 860. From here, the input fuel splits into two directions. One part of the fuel travels “down” through gas permeable felt region 882 and reacts at the anode 820. The fuel reaction products 887 then exit from region 882 through fuel outlet passage 877 in the separator plate 850. Another part of the fuel travels through passage 876 in the electrolyte and passes through the gas permeable region 885 in the cathode conductor/distributor/seal 870. The gas impermeable strip or seal 880 prevents the fuel from entering region 883 and reacting with the oxidizer. The gas impermeable strip or seal 881 prevents the fuel from entering region 884 and contacting the cathode.
  • The input or inlet oxidizer [0230] 888 (dotted-dashed lines in FIG. 46) is provided into oxidizer inlet passage 878 in separator plate 850. The oxidizer passes through the gas permeable region 883 in the anode conductor/distributor/seal 860. The oxidizer then travels through passage 878 in the electrolyte and reaches the gas permeable region 884 in the cathode conductor/distributor/seal 870. From here, the input oxidizer splits into two directions. One part of the oxidizer travels “right” through gas permeable felt region 884 and reacts at the cathode. The reacted oxidizer 889 then travels back and exits from region 884 through oxidizer outlet passage 879 in the separator plate 850. The gas impermeable strip or seal 880 prevents the oxidizer from entering region 882 and contacting the anode. The gas impermeable strip or seal 881 prevents the oxidizer from entering region 885 and reacting with the fuel.
  • The gas [0231] impermeable regions 880, 881 may be formed by any method described in the sixth embodiment, such as by selective heating or laser irradiation or selective addition of a gas impermeable material to the felt. Thus, the gas impermeable regions 880, 881 act as felt seals in the felt conductor/ distributors 860, 870. They separate and prevent the fuel and oxidizer from contacting each other in the fuel cell stack. The fuel stacks and the seals 880, 881 may have any suitable shape and should not be considered limited to the shape illustrated in FIG. 46. Furthermore, “down” and “right” are relative directions depending on the orientation of the fuel cell stack. It should be noted that the fuel and oxidizer cross the fuel stack in different, preferably perpendicular directions.
  • The felt conductor/distributor/seals are not limited to unitary [0232] conductive felt sheets 860, 870 containing both the gas impermeable seals 880, 881 and the gas permeable conductor/ distributors 882, 884. The gas impermeable seals may be formed in separate felt gaskets that are placed adjacent to the gas permeable felt conductor/distributors, as shown in FIG. 47.
  • In FIG. 47, the conductive felt anode conductor/distributor/[0233] seal 890 comprises a gas impermeable felt gasket 891 and a gas permeable felt conductor/distributor 860. The gasket 891 contains a large opening 892, which lines up with the conductor/distributor 860 and with the fuel inlet and outlet passages 876, 877 in the separator plate 850 and the electrolyte 810 (shown in FIG. 46). The inlet fuel enters the conductor/distributor through opening 892 and travels to the anode 820. Alternatively, the one large opening 892 may be replaced with two smaller openings which line up with the conductor/distributor and the fuel passages 876, 877 in the separator plate 850 and electrolyte 810. The gasket 891 also contains the oxidizer inlet and outlet passages 878A, 879A, which do not line up with the anode conductor/distributor 860. Thus, the oxidizer travelling through these passages does not enter the conductor/distributor 860 and does not reach the anode.
  • In FIG. 47, the conductive felt cathode conductor/distributor/[0234] seal 895 comprises a gas impermeable felt gasket 896 and a gas permeable felt conductor/distributor 870. The gasket 896 contains a large opening 897, which lines up with the conductor/distributor 870 and with the oxidizer inlet and outlet passages 878, 879 in the separator plate 850 and the electrolyte 810 (shown in FIG. 46). The inlet oxidizer enters the conductor/distributor through opening 897 and travels to the cathode 830. Alternatively, the one large opening 897 may be replaced with two smaller openings which line up with the conductor/distributor and the oxidizer passages 878, 879 in the separator plate 850 and electrolyte 810. The gasket 896 also contains the fuel inlet and outlet passages 876A, 877A, which do not line up with the cathode conductor/distributor 870. Thus, the fuel travelling through these passages does not enter the conductor/distributor 870 and does not reach the cathode.
  • The conductor/distributor/seals may also be used in externally manifolded fuel cells, as shown in FIG. 48. In FIG. 48, the alternating conductive felt anode and cathode conductor/distributor/seals [0235] 860, 870 are shown as being located in a fuel cell stack housing 899. The housing may have a cylindrical or any other suitable shape. The thin electrolyte, separator plates and electrodes are located between the conductor/distributor/seals 860, 870, but are not shown in FIG. 48 for clarity.
  • The fuel and oxidizer passages are located between the fuel cell stack and the [0236] housing 899. Specifically, passage 876B is a fuel inlet passage, passage 877B is a fuel outlet passage, passage 878B is an oxidizer inlet passage and passage 879B is an oxidizer outlet passage. The “vertical” (i.e., “left” and “right”) surfaces 880A of anode conductor/distributor/seals 860 are rendered gas impermeable. The “horizontal” (i.e., “top” and “bottom”) surfaces 881A of cathode conductor/distributor/seals 870 are also rendered gas impermeable. The remainder of the conductor/distributor/seals 860, 870 remains gas permeable. The sealing may be accomplished by any method described in the sixth embodiment, such as by selective heating or laser irradiation, selective impregnation of the surfaces with a gas impermeable material (i.e., such as by dipping into such material), by selective deposition of foils or thin films on the desired surfaces, or by bending portions of the separator plates around the desired surface edges.
  • The fuel from [0237] passage 876B travels through gas permeable surfaces 882A of sheets 860 to reach the anode. The oxidizer from passage 878B travels through gas permeable surfaces 884A of sheets 870 to reach the cathode. The fuel in passages 876B and 877B does not permeate through surfaces 881A, and does not react with the oxidizer or reach the cathode. The oxidizer in passages 878B and 879B does not permeate through surfaces 880, A and does not react with the fuel or reach the anode.
  • The fuel stacks and the conductor/[0238] distributors 860, 870 may have any suitable shape and should not be considered limited to the shape illustrated in FIG. 48. Furthermore, “vertical” and “horizontal” are relative directions depending on the orientation of the fuel cell stack. It should be noted that the fuel and oxidizer cross the fuel stack in different, preferably perpendicular directions.
  • VIII. Conclusion [0239]
  • The various components of the systems and fuel cells and steps of the methods described in the first through the seventh embodiments may be used together in any combination. Preferably, the components and systems of all seven embodiments are used together. Thus, the preferred method and system include a temperature sensitive adsorption oxygen enrichment method and system of the first embodiment, a load matched power generation system including a solid oxide fuel cell and a heat pump and an optional turbine, and method of using the system of the second embodiment, a textured fuel cell ceramic electrolyte of the third embodiment, an environment tolerant fuel cell anode catalyst of the fourth embodiment, a water vapor replenishment system including the preferred enthalpy wheel of the fifth embodiment, a felt seal in the fuel cell of the sixth embodiment and a felt collector of the seventh embodiment. However, any one, two, three, four or five of the above features may be omitted from the preferred system, fuel cell and method. [0240]
  • The foregoing description of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise form disclosed, and modifications and variations are possible in light of the above teachings or may be acquired from practice of the invention. The drawings are not necessarily to scale and illustrate the device in schematic block format. The drawings and description of the preferred embodiments were chosen in order to explain the principles of the invention and its practical application, and are not meant to be limiting on the scope of the claims. It is intended that the scope of the invention be defined by the claims appended hereto, and their equivalents. [0241]

Claims (21)

What is claimed is:
1. A system comprising:
a solid oxide fuel cell stack; and
an enthalpy wheel which transfers product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply.
2. The system of claim 1, wherein a rotational speed of the enthalpy wheel controls an amount of water vapor provided into the fuel supply.
3. The system of claim 1, wherein up to 90% of the product water vapor is transferred to the fuel supply.
4. The system of claim 1, wherein a hydrocarbon fuel is steam reformed into a hydrogen rich stream within the anode structure of the solid oxide fuel cells of the fuel cell stack.
5. The system of claim 1, further comprising:
a hydrocarbon fuel inlet into the enthalpy wheel;
a heat exchanger which heats the water vapor containing fuel supply with heat from the anode exhaust;
a first conduit between the enthalpy wheel and a first heat exchanger inlet;
a second conduit between a first heat exchanger outlet and the anode inlet;
a third conduit between the anode exhaust and a second heat exchanger inlet; and
a fourth conduit between a second heat exchanger outlet and the enthalpy wheel.
6. The system of claim 5, wherein all heat transferred to the fuel supply is through the enthalpy wheel and the heat exchanger.
7. The system of claim 1, wherein no boiler is used to provide water vapor into the fuel supply during stead state operation of the system.
8. The system of claim 1, further comprising a boiler adapted to provide additional water vapor into the fuel supply.
9. A system comprising:
a solid oxide fuel cell stack; and
at least two adsorbent beds which transfer product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply.
10. The system of claim 9, further comprising:
a hydrocarbon fuel inlet into the at least two adsorbent beds;
a first valve which switches fuel input between a first and a second adsorbent bed;
a heat exchanger which heats the water vapor containing fuel supply with heat from the fuel cell stack anode exhaust;
a first conduit connecting the first adsorbent bed and a first heat exchanger inlet or a first heat exchanger outlet;
a second conduit connecting the second adsorbent bed and the first heat exchanger inlet or the first heat exchanger outlet;
at least one second valve which provides a fluid path between the first adsorbent bed and the first heat exchanger inlet in a second position and between the first adsorbent bed and the first heat exchanger outlet in a first position and which provides a fluid path between the second adsorbent bed and the first heat exchanger outlet in the second position and between the second adsorbent bed and the first heat exchanger inlet in the first position;
a third conduit between a second heat exchanger outlet and the anode inlet; and
a fourth conduit between the anode exhaust and a second heat exchanger inlet.
11. The system of claim 9, further comprising a reformer located between a fuel inlet and the solid oxide fuel cell stack.
12. A system comprising:
a solid oxide fuel cell stack; and
a first means for transferring product water vapor from a fuel cell stack anode exhaust to a fuel cell stack fuel supply.
13. The system of claim 12, further comprising a second means for transferring heat from the fuel cell stack anode exhaust to the fuel cell stack fuel supply.
14. A method of hydrating fuel provided into a solid oxide fuel cell stack, comprising:
providing a hydrocarbon fuel into an anode input of solid oxide fuel cell stack; and
transferring product water vapor from a fuel cell stack anode exhaust into a fuel cell stack fuel supply.
15. The method of claim 14, further comprising transferring heat from the fuel cell stack anode exhaust into the fuel cell stack fuel supply to provide the entire supply of water vapor and heat for the fuel supply to operate the solid oxide fuel cell stack.
16. The method of claim 15, wherein an enthalpy wheel is used to transfer the product water vapor into the fuel supply.
17. The method of claim 16, wherein a heat exchanger is used to transfer the heat from the anode exhaust into the fuel supply.
18. The method of claim 16, further comprising controlling a rotation speed of the enthalpy wheel to control an amount of water vapor added to the fuel supply.
19. The method of claim 18, wherein up to 90% of the water vapor from the anode exhaust is transferred to the fuel supply.
20. The method of claim 14, further comprising:
providing the fuel supply through a first adsorbent bed to transfer at least one of water and water vapor into the fuel supply; and
providing the anode exhaust into a second adsorbent bed to store at least one of water and water vapor in the second adsorbent bed.
21. The method of claim 20, further comprising:
providing the fuel supply through the second adsorbent bed to transfer at least one of water and water vapor into the fuel supply; and
providing the anode exhaust into the first adsorbent bed to store at least one of water and water vapor in the second adsorbent bed.
US10/368,425 2002-02-20 2003-02-20 Fuel water vapor replenishment system for a fuel cell Abandoned US20030162067A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US10/368,425 US20030162067A1 (en) 2002-02-20 2003-02-20 Fuel water vapor replenishment system for a fuel cell

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US35763602P 2002-02-20 2002-02-20
US10/368,425 US20030162067A1 (en) 2002-02-20 2003-02-20 Fuel water vapor replenishment system for a fuel cell

Publications (1)

Publication Number Publication Date
US20030162067A1 true US20030162067A1 (en) 2003-08-28

Family

ID=27757652

Family Applications (7)

Application Number Title Priority Date Filing Date
US10/300,021 Active 2024-06-16 US7067208B2 (en) 2002-02-20 2002-11-20 Load matched power generation system including a solid oxide fuel cell and a heat pump and an optional turbine
US10/368,493 Active 2024-06-09 US7045237B2 (en) 2002-02-20 2003-02-20 Textured electrolyte for a solid oxide fuel cell
US10/368,348 Expired - Lifetime US7255956B2 (en) 2000-03-21 2003-02-20 Environmentally tolerant anode catalyst for a solid oxide fuel cell
US10/369,133 Active 2024-03-31 US7135248B2 (en) 2002-02-20 2003-02-20 Metal felt current conductor and gas flow distributor
US10/369,322 Active 2024-07-28 US7144651B2 (en) 2002-02-20 2003-02-20 High-temperature compliant compression seal
US10/368,425 Abandoned US20030162067A1 (en) 2002-02-20 2003-02-20 Fuel water vapor replenishment system for a fuel cell
US10/369,103 Abandoned US20030170527A1 (en) 2002-02-20 2003-02-20 Temperature sensitive adsorption oxygen enrichment system

Family Applications Before (5)

Application Number Title Priority Date Filing Date
US10/300,021 Active 2024-06-16 US7067208B2 (en) 2002-02-20 2002-11-20 Load matched power generation system including a solid oxide fuel cell and a heat pump and an optional turbine
US10/368,493 Active 2024-06-09 US7045237B2 (en) 2002-02-20 2003-02-20 Textured electrolyte for a solid oxide fuel cell
US10/368,348 Expired - Lifetime US7255956B2 (en) 2000-03-21 2003-02-20 Environmentally tolerant anode catalyst for a solid oxide fuel cell
US10/369,133 Active 2024-03-31 US7135248B2 (en) 2002-02-20 2003-02-20 Metal felt current conductor and gas flow distributor
US10/369,322 Active 2024-07-28 US7144651B2 (en) 2002-02-20 2003-02-20 High-temperature compliant compression seal

Family Applications After (1)

Application Number Title Priority Date Filing Date
US10/369,103 Abandoned US20030170527A1 (en) 2002-02-20 2003-02-20 Temperature sensitive adsorption oxygen enrichment system

Country Status (7)

Country Link
US (7) US7067208B2 (en)
EP (1) EP1497871A4 (en)
JP (1) JP2005518643A (en)
KR (1) KR20040098000A (en)
CN (1) CN1646449A (en)
AU (2) AU2003211129A1 (en)
WO (2) WO2003071619A2 (en)

Cited By (77)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030165732A1 (en) * 2002-02-20 2003-09-04 Ion America Corporation Environmentally tolerant anode catalyst for a solid oxide fuel cell
US20040191598A1 (en) * 2003-03-24 2004-09-30 Ion America Corporation SORFC power and oxygen generation method and system
US20050136299A1 (en) * 2003-12-17 2005-06-23 Richey Joseph B.Ii Oxygen supply system
US20050164051A1 (en) * 2004-01-22 2005-07-28 Ion America Corporation High temperature fuel cell system and method of operating same
US6924053B2 (en) 2003-03-24 2005-08-02 Ion America Corporation Solid oxide regenerative fuel cell with selective anode tail gas circulation
US20060040168A1 (en) * 2004-08-20 2006-02-23 Ion America Corporation Nanostructured fuel cell electrode
US20060210858A1 (en) * 2003-09-29 2006-09-21 Warrier Sunil G Compliant stack for a planar solid oxide fuel cell
US20060228598A1 (en) * 2005-04-07 2006-10-12 Swaminathan Venkataraman Fuel cell system with thermally integrated combustor and corrugated foil reformer
US20060240296A1 (en) * 2005-04-20 2006-10-26 Grieve Malcolm J Regenerable method and system for desulfurizing reformate
US20060251939A1 (en) * 2005-05-09 2006-11-09 Bandhauer Todd M High temperature fuel cell system with integrated heat exchanger network
US20060251940A1 (en) * 2005-05-09 2006-11-09 Bandhauer Todd M High temperature fuel cell system with integrated heat exchanger network
US20060251934A1 (en) * 2005-05-09 2006-11-09 Ion America Corporation High temperature fuel cell system with integrated heat exchanger network
US20060257696A1 (en) * 2005-05-10 2006-11-16 Ion America Corporation Increasing thermal dissipation of fuel cell stacks under partial electrical load
US20070017369A1 (en) * 2005-07-25 2007-01-25 Ion America Corporation Fuel cell anode exhaust fuel recovery by adsorption
US20070017367A1 (en) * 2005-07-25 2007-01-25 Ion America Corporation Partial pressure swing adsorption system for providing hydrogen to a vehicle fuel cell
US20070017368A1 (en) * 2005-07-25 2007-01-25 Ion America Corporation Gas separation method and apparatus using partial pressure swing adsorption
US20070178338A1 (en) * 2005-07-25 2007-08-02 Ion America Corporation Fuel cell system with electrochemical anode exhaust recycling
US20070196702A1 (en) * 2003-04-09 2007-08-23 Bloom Energy Corporation Low pressure hydrogen fueled vehicle and method of operating same
US20070231631A1 (en) * 2006-04-03 2007-10-04 Bloom Energy Corporation Hybrid reformer for fuel flexibility
US20070231635A1 (en) * 2006-04-03 2007-10-04 Bloom Energy Corporation Fuel cell system operated on liquid fuels
US20070238007A1 (en) * 2006-03-30 2007-10-11 Shinko Electric Industries Co., Ltd. Solid electrolyte fuel cell and process for the production thereof
US20070259225A1 (en) * 2006-04-21 2007-11-08 Michael Penev Recovering a reactant from a fuel cell exhaust flow
US7306641B2 (en) * 2003-09-12 2007-12-11 Hewlett-Packard Development Company, L.P. Integral fuel cartridge and filter
US20080057359A1 (en) * 2006-09-06 2008-03-06 Bloom Energy Corporation Flexible fuel cell system configuration to handle multiple fuels
US20080076006A1 (en) * 2006-09-25 2008-03-27 Ion America Corporation High utilization stack
US20080096080A1 (en) * 2006-10-18 2008-04-24 Bloom Energy Corporation Anode with remarkable stability under conditions of extreme fuel starvation
US20080096073A1 (en) * 2006-10-23 2008-04-24 Bloom Energy Corporation Dual function heat exchanger for start-up humidification and facility heating in SOFC system
US7364810B2 (en) 2003-09-03 2008-04-29 Bloom Energy Corporation Combined energy storage and fuel generation with reversible fuel cells
US20080152959A1 (en) * 2006-12-20 2008-06-26 Bloom Energy Corporation Methods for fuel cell system optimization
US20080241638A1 (en) * 2007-03-30 2008-10-02 Bloom Energy Corporation SOFC system producing reduced atmospheric carbon dioxide using a molten carbonated carbon dioxide pump
US20080241612A1 (en) * 2007-03-30 2008-10-02 Bloom Energy Corporation Fuel cell system with one hundred percent fuel utilization
US20080254336A1 (en) * 2007-04-13 2008-10-16 Bloom Energy Corporation Composite anode showing low performance loss with time
US20080261099A1 (en) * 2007-04-13 2008-10-23 Bloom Energy Corporation Heterogeneous ceramic composite SOFC electrolyte
US20080318092A1 (en) * 2003-04-09 2008-12-25 Bloom Energy Corporation Co-production of hydrogen and electricity in a high temperature electrochemical system
US7575822B2 (en) 2003-04-09 2009-08-18 Bloom Energy Corporation Method of optimizing operating efficiency of fuel cells
US20090208785A1 (en) * 2008-02-20 2009-08-20 Bloom Energy Cororation SOFC electrochemical anode tail gas oxidizer
US20090208784A1 (en) * 2008-02-19 2009-08-20 Bloom Energy Corporation Fuel cell system containing anode tail gas oxidizer and hybrid heat exchanger/reformer
US20100028736A1 (en) * 2008-08-01 2010-02-04 Georgia Tech Research Corporation Hybrid Ionomer Electrochemical Devices
US7659022B2 (en) 2006-08-14 2010-02-09 Modine Manufacturing Company Integrated solid oxide fuel cell and fuel processor
US20100047637A1 (en) * 2008-07-23 2010-02-25 Bloom Energy Corporation Operation of fuel cell systems with reduced carbon formation and anode leading edge damage
US20100107435A1 (en) * 2008-10-31 2010-05-06 Jacob George Methods and Apparatus for Drying Ceramic Green Bodies with Microwaves
US20100183930A1 (en) * 2009-01-20 2010-07-22 Adaptive Materials, Inc. Method for controlling a water based fuel reformer
US20100239924A1 (en) * 2005-07-25 2010-09-23 Ion America Corporation Fuel cell system with partial recycling of anode exhaust
US7846599B2 (en) 2007-06-04 2010-12-07 Bloom Energy Corporation Method for high temperature fuel cell system start up and shutdown
US20110039183A1 (en) * 2009-08-12 2011-02-17 Bloom Energy Corporation Internal reforming anode for solid oxide fuel cells
US20110053027A1 (en) * 2009-09-02 2011-03-03 Bloom Energy Corporation Multi-Stream Heat Exchanger for a Fuel Cell System
US20110171544A1 (en) * 2008-09-19 2011-07-14 Mtu Onsite Energy Gmbh Fuel cell assembly with improved gas recirculation
US20110183233A1 (en) * 2010-01-26 2011-07-28 Bloom Energy Corporation Phase Stable Doped Zirconia Electrolyte Compositions with Low Degradation
US20110189572A1 (en) * 2009-01-30 2011-08-04 Adaptive Materials, Inc. Fuel cell system with flame protection member
US20110189578A1 (en) * 2010-02-01 2011-08-04 Adaptive Materials, Inc. Fuel cell system including a resilient manifold interconnecting member
US8067129B2 (en) 2007-11-13 2011-11-29 Bloom Energy Corporation Electrolyte supported cell designed for longer life and higher power
US8137855B2 (en) 2007-07-26 2012-03-20 Bloom Energy Corporation Hot box design with a multi-stream heat exchanger and single air control
US20120077099A1 (en) * 2010-09-23 2012-03-29 Adaptive Materials, Inc. Solid oxide fuel cell with multiple fuel streams
US8241801B2 (en) 2006-08-14 2012-08-14 Modine Manufacturing Company Integrated solid oxide fuel cell and fuel processor
US20120264029A1 (en) * 2011-04-14 2012-10-18 Hitachi, Ltd. Fuel cell system
US8440362B2 (en) 2010-09-24 2013-05-14 Bloom Energy Corporation Fuel cell mechanical components
WO2013085216A1 (en) * 2011-12-05 2013-06-13 두산중공업 주식회사 Fuel cell system and method for driving same
US8563180B2 (en) 2011-01-06 2013-10-22 Bloom Energy Corporation SOFC hot box components
US8796888B2 (en) 2010-07-07 2014-08-05 Adaptive Materials, Inc. Wearable power management system
US8852820B2 (en) 2007-08-15 2014-10-07 Bloom Energy Corporation Fuel cell stack module shell with integrated heat exchanger
US8968958B2 (en) 2008-07-08 2015-03-03 Bloom Energy Corporation Voltage lead jumper connected fuel cell columns
US9190693B2 (en) 2006-01-23 2015-11-17 Bloom Energy Corporation Modular fuel cell system
US9216405B1 (en) * 2014-06-26 2015-12-22 Kraton Polymers U.S. Llc Rotary enthalpy exchange wheel having sulfonated block copolymer
US9246184B1 (en) 2007-11-13 2016-01-26 Bloom Energy Corporation Electrolyte supported cell designed for longer life and higher power
US9287572B2 (en) 2013-10-23 2016-03-15 Bloom Energy Corporation Pre-reformer for selective reformation of higher hydrocarbons
US9461320B2 (en) 2014-02-12 2016-10-04 Bloom Energy Corporation Structure and method for fuel cell system where multiple fuel cells and power electronics feed loads in parallel allowing for integrated electrochemical impedance spectroscopy (EIS)
US9515344B2 (en) 2012-11-20 2016-12-06 Bloom Energy Corporation Doped scandia stabilized zirconia electrolyte compositions
US9755263B2 (en) 2013-03-15 2017-09-05 Bloom Energy Corporation Fuel cell mechanical components
US10347930B2 (en) 2015-03-24 2019-07-09 Bloom Energy Corporation Perimeter electrolyte reinforcement layer composition for solid oxide fuel cell electrolytes
US10615444B2 (en) 2006-10-18 2020-04-07 Bloom Energy Corporation Anode with high redox stability
US10651496B2 (en) 2015-03-06 2020-05-12 Bloom Energy Corporation Modular pad for a fuel cell system
US10680251B2 (en) 2017-08-28 2020-06-09 Bloom Energy Corporation SOFC including redox-tolerant anode electrode and system including the same
US11322767B2 (en) 2019-04-12 2022-05-03 Bloom Energy Corporation Solid oxide fuel cell system with hydrogen pumping cell with carbon monoxide tolerant anodes and integrated shift reactor
US11398634B2 (en) 2018-03-27 2022-07-26 Bloom Energy Corporation Solid oxide fuel cell system and method of operating the same using peak shaving gas
EP4071867A3 (en) * 2021-04-08 2022-11-09 Bloom Energy Corporation Hydrogen pumping proton exchange membrane electrochemical cell with carbon monoxide tolerant anode and method of making thereof
EP4147768A1 (en) * 2021-09-10 2023-03-15 Hamilton Sundstrand Corporation Water recovery system for fuel cells
US11616249B2 (en) 2019-03-22 2023-03-28 Bloom Energy Corporation Solid oxide fuel cell system with hydrogen pumping cell with carbon monoxide tolerant anodes and integrated shift reactor

Families Citing this family (207)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030194592A1 (en) * 2002-04-10 2003-10-16 Hilliard Donald Bennett Solid oxide electrolytic device
US20030215689A1 (en) * 2002-05-16 2003-11-20 Keegan Kevin R. Solid oxide fuel cell with a metal foam seal
AU2003250671A1 (en) * 2002-07-23 2004-02-09 Global Thermoelectric Inc. High temperature gas seals
WO2004021497A2 (en) * 2002-08-07 2004-03-11 Battelle Memorial Institute Passive vapor exchange systems and techniques for fuel reforming and prevention of carbon fouling
WO2004105154A2 (en) * 2002-08-13 2004-12-02 Ztek Corporation Method of forming freestanding thin chromium components for an electrochemical converter
US7112296B2 (en) * 2002-10-18 2006-09-26 Hewlett-Packard Development Company, L.P. Method for making thin fuel cell electrolyte
DE10324157B3 (en) * 2003-05-22 2004-08-19 Reinz-Dichtungs-Gmbh & Co. Kg High temperature fuel cell system include resilient channel configurations which sealing openings and are located in electrically-active regions of fuel cell stack
US7531261B2 (en) * 2003-06-30 2009-05-12 Corning Incorporated Textured electrolyte sheet for solid oxide fuel cell
US7113146B2 (en) * 2003-06-30 2006-09-26 The Boeing Company Broadband monopole
EP1665431B1 (en) * 2003-09-08 2015-10-07 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Interconnector for high-temperature fuel cell unit
US20060166070A1 (en) * 2003-09-10 2006-07-27 Ion America Corporation Solid oxide reversible fuel cell with improved electrode composition
US20050058867A1 (en) * 2003-09-15 2005-03-17 Intel Corporation Integrated platform and fuel cell cooling
US20050058866A1 (en) * 2003-09-15 2005-03-17 Intel Corporation Integrated platform and fuel cell cooling
US7160641B2 (en) * 2003-10-24 2007-01-09 General Motors Corporation Methods to cool a fuel cell and if desired heat a hybrid bed simultaneously
US7410716B2 (en) * 2003-11-03 2008-08-12 Corning Incorporated Electrolyte sheet with protruding features having undercut angles and method of separating such sheet from its carrier
EP1695407A1 (en) * 2003-12-17 2006-08-30 Greenlight Power Technologies, Inc. System and method for treating process fluids delivered to an electrochemical cell stack
JP2005190684A (en) * 2003-12-24 2005-07-14 Toyota Motor Corp Fuel cell
US20050221163A1 (en) * 2004-04-06 2005-10-06 Quanmin Yang Nickel foam and felt-based anode for solid oxide fuel cells
KR100589408B1 (en) 2004-04-29 2006-06-14 삼성에스디아이 주식회사 Fuel cell system
US20050244241A1 (en) * 2004-04-30 2005-11-03 Joichi Miyazaki Cooling system, cooling method, and electronic apparatus
US7638226B2 (en) * 2004-07-13 2009-12-29 Ford Motor Company Apparatus and method for controlling kinetic rates for internal reforming of fuel in solid oxide fuel cells
US7024800B2 (en) 2004-07-19 2006-04-11 Earthrenew, Inc. Process and system for drying and heat treating materials
US7685737B2 (en) * 2004-07-19 2010-03-30 Earthrenew, Inc. Process and system for drying and heat treating materials
US7422819B2 (en) * 2004-12-30 2008-09-09 Delphi Technologies, Inc. Ceramic coatings for insulating modular fuel cell cassettes in a solid-oxide fuel cell stack
US20060147771A1 (en) * 2005-01-04 2006-07-06 Ion America Corporation Fuel cell system with independent reformer temperature control
US20060166159A1 (en) 2005-01-25 2006-07-27 Norbert Abels Laser shaping of green metal body used in manufacturing an orthodontic bracket
US20060163774A1 (en) * 2005-01-25 2006-07-27 Norbert Abels Methods for shaping green bodies and articles made by such methods
US20060188649A1 (en) * 2005-02-22 2006-08-24 General Electric Company Methods of sealing solid oxide fuel cells
US7713649B2 (en) * 2005-03-10 2010-05-11 Bloom Energy Corporation Fuel cell stack with internal fuel manifold configuration
CA2601981A1 (en) * 2005-03-24 2006-09-28 Ohio University Sulphur-tolerant anode for solid oxide fuel cell
JP2006286439A (en) * 2005-04-01 2006-10-19 Matsushita Electric Ind Co Ltd Fuel cell generator
US20060248799A1 (en) * 2005-05-09 2006-11-09 Bandhauer Todd M High temperature fuel cell system with integrated heat exchanger network
WO2006125177A2 (en) * 2005-05-19 2006-11-23 Massachusetts Institute Of Technology Electrode and catalytic materials
FR2887371A1 (en) * 2005-06-21 2006-12-22 Renault Sas Electrical energy producing system for propulsion of motor vehicle, has fuel cell device with stack of individual cells and reformer device associated to burner, and oxygenation device oxygenating airflow supplying fuel cell device
JP4555171B2 (en) * 2005-06-24 2010-09-29 本田技研工業株式会社 Fuel cell and fuel cell stack
JP4555170B2 (en) * 2005-06-24 2010-09-29 本田技研工業株式会社 Fuel cell and fuel cell stack
JP4555173B2 (en) * 2005-06-24 2010-09-29 本田技研工業株式会社 Fuel cell and fuel cell stack
JP4555172B2 (en) * 2005-06-24 2010-09-29 本田技研工業株式会社 Fuel cell and fuel cell stack
KR100728781B1 (en) * 2005-07-27 2007-06-19 삼성에스디아이 주식회사 Membrane-electrode assembly for fuel cell and fuel cell system comprising same
US20070072046A1 (en) * 2005-09-26 2007-03-29 General Electric Company Electrochemcial cell structures and methods of making the same
US9985295B2 (en) * 2005-09-26 2018-05-29 General Electric Company Solid oxide fuel cell structures, and related compositions and processes
US20070072070A1 (en) * 2005-09-26 2007-03-29 General Electric Company Substrates for deposited electrochemical cell structures and methods of making the same
US8142943B2 (en) * 2005-11-16 2012-03-27 Bloom Energy Corporation Solid oxide fuel cell column temperature equalization by internal reforming and fuel cascading
US8097374B2 (en) * 2005-11-16 2012-01-17 Bloom Energy Corporation System and method for providing reformed fuel to cascaded fuel cell stacks
DE102005054888B4 (en) * 2005-11-17 2009-12-10 Airbus Deutschland Gmbh Oxygenating device in combination with a fuel cell system and use
US7931990B2 (en) * 2005-12-15 2011-04-26 Saint-Gobain Ceramics & Plastics, Inc. Solid oxide fuel cell having a buffer layer
US20070141422A1 (en) * 2005-12-16 2007-06-21 Saint-Gobain Ceramics & Plastics, Inc. Fuel cell component having an electrolyte dopant
US7610692B2 (en) 2006-01-18 2009-11-03 Earthrenew, Inc. Systems for prevention of HAP emissions and for efficient drying/dehydration processes
JP5103757B2 (en) * 2006-03-08 2012-12-19 トヨタ自動車株式会社 Fuel cell oxidant gas purification device
WO2007112435A2 (en) * 2006-03-28 2007-10-04 Ohio University Solid oxide fuel cell process and apparatus
JP2007265920A (en) * 2006-03-29 2007-10-11 Dainippon Printing Co Ltd Solid oxide fuel cell and its manufacturing method
JP5007918B2 (en) * 2006-03-30 2012-08-22 日産自動車株式会社 Gas seal part for fuel cell and manufacturing method thereof
US8691474B2 (en) * 2006-04-03 2014-04-08 Bloom Energy Corporation Fuel cell stack components and materials
US7951509B2 (en) * 2006-04-03 2011-05-31 Bloom Energy Corporation Compliant cathode contact materials
JP5177474B2 (en) * 2006-04-24 2013-04-03 日本碍子株式会社 Ceramic thin plate
JP5154030B2 (en) * 2006-05-18 2013-02-27 本田技研工業株式会社 Fuel cell system and operation method thereof
US8216738B2 (en) * 2006-05-25 2012-07-10 Versa Power Systems, Ltd. Deactivation of SOFC anode substrate for direct internal reforming
US20080023322A1 (en) * 2006-07-27 2008-01-31 Sinuc Robert A Fuel processor
US20080032178A1 (en) * 2006-08-02 2008-02-07 Phong Diep Solid oxide fuel cell device with an elongated seal geometry
JP5198000B2 (en) * 2006-09-14 2013-05-15 本田技研工業株式会社 Electrolyte / electrode assembly and method for producing the same
US9190669B2 (en) 2006-10-02 2015-11-17 Versa Power Systems, Ltd. Cell materials variation in SOFC stacks to address thermal gradients in all planes
US8313875B2 (en) * 2006-10-02 2012-11-20 Versa Power Systems, Ltd. High performance cathode with controlled operating temperature range
KR20090082263A (en) 2006-10-31 2009-07-29 코닝 인코포레이티드 Micromachined electrolyte sheet, fuel cell devices utilizing such, and micromachining method for making fuel cell devices
GB0621784D0 (en) * 2006-11-01 2006-12-13 Ceres Power Ltd Fuel cell heat exchange systems and methods
AU2007315974B2 (en) * 2006-11-01 2012-06-28 Ceres Intellectual Property Company Limited Fuel cell heat exchange systems and methods
US8197979B2 (en) * 2006-12-12 2012-06-12 Corning Incorporated Thermo-mechanical robust seal structure for solid oxide fuel cells
US20080145746A1 (en) * 2006-12-19 2008-06-19 General Electric Company Copper-based energy storage device and method
CN102244304A (en) * 2006-12-19 2011-11-16 通用电气公司 Copper-based energy storage device and method
US20080199738A1 (en) * 2007-02-16 2008-08-21 Bloom Energy Corporation Solid oxide fuel cell interconnect
AU2008234276B2 (en) * 2007-04-02 2010-08-26 Sunfire Gmbh Contact arrangement and method for assembling a fuel cell stack from at least one contact arrangement
US20080260455A1 (en) * 2007-04-17 2008-10-23 Air Products And Chemicals, Inc. Composite Seal
US7781120B2 (en) 2007-05-16 2010-08-24 Corning Incorporated Thermo-mechanical robust solid oxide fuel cell device assembly
US20090081512A1 (en) 2007-09-25 2009-03-26 William Cortez Blanchard Micromachined electrolyte sheet, fuel cell devices utilizing such, and micromachining method for making fuel cell devices
FR2922047A1 (en) * 2007-10-09 2009-04-10 Commissariat Energie Atomique PROCESS FOR TEXTURING THE ELECTROLYTE OF A FUEL CELL
AT505416B1 (en) * 2007-10-22 2009-01-15 Vaillant Austria Gmbh HIGH TEMPERATURE FUEL CELL WITH ADSORPTION HEAT PUMP
EP2215680A4 (en) * 2007-10-29 2012-03-14 Utc Power Corp Integration of an organic rankine cycle with a fuel cell
WO2009058110A1 (en) * 2007-10-29 2009-05-07 Utc Power Corporation Method and apparatus for operating a fuel cell in combination with an orc system
WO2009061292A1 (en) * 2007-11-06 2009-05-14 Carrier Corporation Heat pump with heat recovery
EP2231306B1 (en) * 2007-11-12 2014-02-12 ExxonMobil Upstream Research Company Methods of generating and utilizing utility gas
US20090142639A1 (en) * 2007-11-29 2009-06-04 Steven Joseph Gregorski Seal system for solid oxide fuel cell and method of making
JP5228457B2 (en) * 2007-11-30 2013-07-03 大日本印刷株式会社 Method for producing solid oxide fuel cell
US7815843B2 (en) * 2007-12-27 2010-10-19 Institute Of Nuclear Energy Research Process for anode treatment of solid oxide fuel cell—membrane electrode assembly to upgrade power density in performance test
EP2249422A4 (en) * 2008-01-29 2013-01-02 Kyocera Corp Fuel cell module and fuel cell device
US7931997B2 (en) * 2008-03-12 2011-04-26 Bloom Energy Corporation Multi-material high temperature fuel cell seals
EP2104172A1 (en) * 2008-03-20 2009-09-23 The Technical University of Denmark A composite glass seal for a solid oxide electrolyser cell stack
US8623301B1 (en) 2008-04-09 2014-01-07 C3 International, Llc Solid oxide fuel cells, electrolyzers, and sensors, and methods of making and using the same
WO2009134543A1 (en) 2008-04-30 2009-11-05 Exxonmobil Upstream Research Company Method and apparatus for removal of oil from utility gas stream
EP2297807A1 (en) * 2008-06-17 2011-03-23 Battelle Memorial Institute Sofc double seal with dimensional control for superior thermal cycle stability
DE102008045286B4 (en) * 2008-08-04 2010-07-15 Mtu Onsite Energy Gmbh A method of making porous molten carbonate fuel cell anodes and green molten carbonate fuel cell anode
US20100055508A1 (en) * 2008-08-27 2010-03-04 Idatech, Llc Fuel cell systems with water recovery from fuel cell effluent
US8310157B2 (en) * 2008-09-10 2012-11-13 General Electric Company Lamp having metal conductor bonded to ceramic leg member
FR2935843B1 (en) * 2008-09-11 2011-02-11 Commissariat Energie Atomique ELECTROLYTE FOR SOFC CELL AND METHOD FOR MANUFACTURING THE SAME
AU2009301640B2 (en) 2008-10-09 2014-12-04 Chaozhou Three-Circle (Group) Co., Ltd. A solid oxide fuel cell or solid oxide fuel cell sub-component and methods of preparing same
FR2938121B1 (en) 2008-10-30 2011-04-01 Commissariat Energie Atomique ELECTROLYTE PLATE WITH INCREASED RIGIDITY, AND ELECTROCHEMICAL SYSTEM COMPRISING SUCH AN ELECTROLYTE PLATE
US8986905B2 (en) * 2008-11-11 2015-03-24 Bloom Energy Corporation Fuel cell interconnect
US8623569B2 (en) 2008-12-09 2014-01-07 Bloom Energy Corporation Fuel cell seals
US8268504B2 (en) * 2008-12-22 2012-09-18 General Electric Company Thermomechanical sealing of interconnect manifolds in fuel cell stacks
US8146374B1 (en) 2009-02-13 2012-04-03 Source IT Energy, LLC System and method for efficient utilization of energy generated by a utility plant
DE102009009675A1 (en) * 2009-02-19 2010-08-26 Daimler Ag Fuel cell system with at least one fuel cell
DE102009009673A1 (en) * 2009-02-19 2010-08-26 Daimler Ag Fuel cell system with at least one fuel cell
DE102009009674A1 (en) * 2009-02-19 2010-08-26 Daimler Ag Fuel cell system with at least one fuel cell
US8652697B2 (en) 2009-02-25 2014-02-18 Bloom Energy Corporation Controlling a fuel cell system based on fuel cell impedance characteristic
US8663869B2 (en) * 2009-03-20 2014-03-04 Bloom Energy Corporation Crack free SOFC electrolyte
EP2433904B1 (en) * 2009-05-20 2019-11-20 Panasonic Corporation Method for operating a hydrogen generation device and fuel cell system
US8535836B2 (en) 2009-07-08 2013-09-17 Bloom Energy Corporation Method of operating a fuel cell system with bypass ports in a fuel processing assembly
GB2473550B (en) * 2009-09-11 2012-03-28 Univ Washington State Res Fdn Catalyst materials and methods for reforming hydrocarbon fuels
FR2951517B1 (en) * 2009-10-20 2011-12-09 Commissariat Energie Atomique SEAL SEAL BETWEEN TWO ELEMENTS WITH DIFFERENT THERMAL EXPANSION COEFFICIENTS
EP2325931A1 (en) * 2009-11-18 2011-05-25 Plansee Se Assembly for a fuel cell and method for producing same
ES2360439B8 (en) * 2009-11-25 2012-10-30 CONSEJO SUPERIOR DE INVESTIGACIONES CIENTÍFICAS (CSIC) (Titular al 60%) SYSTEM AND PROCEDURE FOR THE MANUFACTURE OF ELECTROLYTIC MEMBERS THIN AND SELF-SUPPORTED BY LASER MACHINING.
RU2012132260A (en) 2009-12-28 2014-02-10 Сосьете Бик FUEL ELEMENTS AND COMPONENTS OF FUEL ELEMENTS, ASYMMETRIC ARCHITECTURE, AND METHODS FOR THEIR MANUFACTURE
CA2789281C (en) 2010-02-10 2015-11-24 C3 International, Llc Low temperature electrolytes for solid oxide cells having high ionic conductivity
EP2555296B1 (en) * 2010-03-30 2016-11-23 Nippon Shokubai Co., Ltd. Electrolyte sheet for solid oxide type fuel cell and process for production thereof, single cell for solid oxide type fuel cell, and solid oxide type fuel cell
JP5889288B2 (en) 2010-05-28 2016-03-22 エクソンモービル アップストリーム リサーチ カンパニー Integrated adsorber head and valve design and associated swing adsorption method
US8529202B2 (en) * 2010-10-12 2013-09-10 General Electric Company System and method for turbine compartment ventilation
TWI495501B (en) 2010-11-15 2015-08-11 Exxonmobil Upstream Res Co Kinetic fractionators, and cycling processes for fractionation of gas mixtures
KR101161992B1 (en) 2010-12-28 2012-07-03 주식회사 포스코 Method for manufacturing multi-layered sealant for solid oxide fuel cell
US9017457B2 (en) 2011-03-01 2015-04-28 Exxonmobil Upstream Research Company Apparatus and systems having a reciprocating valve head assembly and swing adsorption processes related thereto
WO2012161826A1 (en) 2011-03-01 2012-11-29 Exxonmobil Upstream Research Company Methods of removing contaminants from a hydrocarbon stream by swing adsorption and related apparatus and systems
US9162175B2 (en) 2011-03-01 2015-10-20 Exxonmobil Upstream Research Company Apparatus and systems having compact configuration multiple swing adsorption beds and methods related thereto
MY173802A (en) 2011-03-01 2020-02-24 Exxonmobil Upstream Res Co Apparatus and systems having an encased adsorbent contractor and swing adsorption processes related thereto
EA201391249A1 (en) 2011-03-01 2014-02-28 Эксонмобил Апстрим Рисерч Компани DEVICES AND SYSTEMS HAVING A KING VALVE, AND RELATED CYCLIC ADSORPTION PROCESSES
CA2842928A1 (en) 2011-03-01 2012-11-29 Exxonmobil Upstream Research Company Apparatus and systems having a rotary valve assembly and swing adsorption processes related thereto
MY163007A (en) 2011-03-01 2017-07-31 Exxonmobil Upstream Res Co Methods of removing contaminants from hydrocarbon stream by swing adsorption and related apparatus and systems
JP5686182B2 (en) * 2011-03-24 2015-03-18 株式会社村田製作所 Solid oxide fuel cell bonding material, solid oxide fuel cell, and solid oxide fuel cell module
WO2012133086A1 (en) * 2011-03-25 2012-10-04 株式会社村田製作所 Bonding member for solid oxide fuel cell, solid oxide fuel cell, and solid oxide fuel cell module
WO2012133087A1 (en) * 2011-03-30 2012-10-04 株式会社村田製作所 Bonding member for solid oxide fuel cell, solid oxide fuel cell, and solid oxide fuel cell module
JP5686190B2 (en) * 2011-07-21 2015-03-18 株式会社村田製作所 Joining material for solid oxide fuel cell, method for producing solid oxide fuel cell, method for producing solid oxide fuel cell module, solid oxide fuel cell and solid oxide fuel cell module
GB2494400B (en) * 2011-09-06 2017-11-22 Highview Entpr Ltd Method and apparatus for power storage
TWI552417B (en) 2011-11-17 2016-10-01 博隆能源股份有限公司 Multi-layered coating providing corrosion resistance to zirconia based electrolytes
US8962219B2 (en) 2011-11-18 2015-02-24 Bloom Energy Corporation Fuel cell interconnects and methods of fabrication
US9452475B2 (en) 2012-03-01 2016-09-27 Bloom Energy Corporation Coatings for SOFC metallic interconnects
US9847520B1 (en) 2012-07-19 2017-12-19 Bloom Energy Corporation Thermal processing of interconnects
US9759456B2 (en) 2012-08-02 2017-09-12 Trane International Inc. Combined heat and power heat pump
WO2014036058A1 (en) 2012-08-29 2014-03-06 Bloom Energy Corporation Interconnect for fuel cell stack
US9034078B2 (en) 2012-09-05 2015-05-19 Exxonmobil Upstream Research Company Apparatus and systems having an adsorbent contactor and swing adsorption processes related thereto
US9478812B1 (en) 2012-10-17 2016-10-25 Bloom Energy Corporation Interconnect for fuel cell stack
JP6071430B2 (en) * 2012-10-31 2017-02-01 三菱日立パワーシステムズ株式会社 Power generation system and method for operating power generation system
CN104769762A (en) 2012-11-06 2015-07-08 博隆能源股份有限公司 Improved interconnect and end plate design for fuel cell stack
US9276301B2 (en) 2012-12-07 2016-03-01 Samsung Electronics Co., Ltd. Polymeric compound, oxygen permeable membrane, and electrochemical device
US9343786B2 (en) 2012-12-10 2016-05-17 Samsung Electronics Co., Ltd. Electrochemical device
TWI491794B (en) * 2012-12-18 2015-07-11 Nat Univ Tsing Hua And a method for producing an exhaust gas purifying reactor in which a plurality of layers are arranged
WO2014126716A1 (en) 2013-02-13 2014-08-21 Phillips 66 Company Electrolyte formation for a solid oxide fuel cell device
US8968509B2 (en) 2013-05-09 2015-03-03 Bloom Energy Corporation Methods and devices for printing seals for fuel cell stacks
TWI621302B (en) 2013-05-16 2018-04-11 博隆能源股份有限公司 Corrosion resistant barrier layer for a solid oxide fuel cell stack and method of making thereof
EP3022792A4 (en) 2013-07-15 2016-12-21 Fcet Inc Low temperature solid oxide cells
EP3053211A4 (en) 2013-10-01 2017-07-05 Bloom Energy Corporation Pre-formed powder delivery to powder press machine
US10418657B2 (en) 2013-10-08 2019-09-17 Phillips 66 Company Formation of solid oxide fuel cells by spraying
US9666891B2 (en) 2013-10-08 2017-05-30 Phillips 66 Company Gas phase modification of solid oxide fuel cells
US9660273B2 (en) 2013-10-08 2017-05-23 Phillips 66 Company Liquid phase modification of solid oxide fuel cells
WO2015080889A1 (en) 2013-11-27 2015-06-04 Bloom Energy Corporation Fuel cell interconnect with reduced voltage degradation over time
US9859580B2 (en) 2014-01-06 2018-01-02 Bloom Energy Corporation Structure and method for indicating undesirable constituents in a fuel cell system
US10079393B1 (en) 2014-01-09 2018-09-18 Bloom Energy Corporation Method of fabricating an interconnect for a fuel cell stack
US9461319B2 (en) 2014-02-21 2016-10-04 Bloom Energy Corporation Electrochemical impedance spectroscopy (EIS) analyzer and method of using thereof
WO2015130644A1 (en) 2014-02-25 2015-09-03 Bloom Energy Corporation Composition and processing of metallic interconnects for sofc stacks
US9559366B2 (en) * 2014-03-20 2017-01-31 Versa Power Systems Ltd. Systems and methods for preventing chromium contamination of solid oxide fuel cells
US9923211B2 (en) 2014-04-24 2018-03-20 Bloom Energy Corporation Fuel cell interconnect with reduced voltage degradation over time
US9675925B2 (en) 2014-07-25 2017-06-13 Exxonmobil Upstream Research Company Apparatus and system having a valve assembly and swing adsorption processes related thereto
RU2699551C2 (en) 2014-11-11 2019-09-06 Эксонмобил Апстрим Рисерч Компани High-capacity structures and monoliths via paste imprinting
US9713787B2 (en) 2014-12-10 2017-07-25 Exxonmobil Upstream Research Company Adsorbent-incorporated polymer fibers in packed bed and fabric contactors, and methods and devices using same
SG10201912671YA (en) 2014-12-23 2020-03-30 Exxonmobil Upstream Res Co Structured adsorbent beds, methods of producing the same and uses thereof
JP6474065B2 (en) * 2014-12-26 2019-02-27 株式会社日本触媒 Electrolyte sheet for solid oxide fuel cell
US9789536B2 (en) 2015-01-20 2017-10-17 United Technologies Corporation Dual investment technique for solid mold casting of reticulated metal foams
US9737930B2 (en) 2015-01-20 2017-08-22 United Technologies Corporation Dual investment shelled solid mold casting of reticulated metal foams
US9789534B2 (en) 2015-01-20 2017-10-17 United Technologies Corporation Investment technique for solid mold casting of reticulated metal foams
JP6546398B2 (en) * 2015-01-23 2019-07-17 東京瓦斯株式会社 Fuel cell system
US10381698B2 (en) * 2015-04-29 2019-08-13 Samsung Electronics Co., Ltd. Metal air battery having air purification module, electrochemical cell having air purification module and method of operating metal air battery
AU2016265109B2 (en) 2015-05-15 2019-03-07 Exxonmobil Upstream Research Company Apparatus and system for swing adsorption processes related thereto comprising mid-bed purge systems
SG11201707065PA (en) 2015-05-15 2017-11-29 Exxonmobil Upstream Res Co Apparatus and system for swing adsorption processes related thereto
US9884363B2 (en) 2015-06-30 2018-02-06 United Technologies Corporation Variable diameter investment casting mold for casting of reticulated metal foams
US9731342B2 (en) 2015-07-07 2017-08-15 United Technologies Corporation Chill plate for equiax casting solidification control for solid mold casting of reticulated metal foams
US10080991B2 (en) 2015-09-02 2018-09-25 Exxonmobil Upstream Research Company Apparatus and system for swing adsorption processes related thereto
EP3344371B1 (en) 2015-09-02 2021-09-15 ExxonMobil Upstream Research Company Process and system for swing adsorption using an overhead stream of a demethanizer as purge gas
US10573910B2 (en) 2015-09-14 2020-02-25 Bloom Energy Corporation Electrochemical impedance spectroscopy (“EIS”) analyzer and method of using thereof
US10320017B2 (en) 2015-10-06 2019-06-11 Bloom Energy Corporation Sorbent bed assembly and fuel cell system including same
US10040022B2 (en) 2015-10-27 2018-08-07 Exxonmobil Upstream Research Company Apparatus and system for swing adsorption processes related thereto
EP3368188A1 (en) 2015-10-27 2018-09-05 Exxonmobil Upstream Research Company Apparatus and system for swing adsorption processes related thereto having a plurality of valves
EA201891043A1 (en) 2015-10-27 2018-10-31 Эксонмобил Апстрим Рисерч Компани DEVICE AND SYSTEM FOR IMPLEMENTATION OF SHORT-CYCLIC ADSORPTION PROCESSES AND METHOD REQUIRING THEM
EP3377194A1 (en) 2015-11-16 2018-09-26 Exxonmobil Upstream Research Company Adsorbent materials and methods of adsorbing carbon dioxide
ITUB20161137A1 (en) * 2016-02-26 2017-08-26 Claudio Merler TRIGENERATIVE SYSTEM WITH FIRST CELL FUEL GENERATOR
JP2019508245A (en) 2016-03-18 2019-03-28 エクソンモービル アップストリーム リサーチ カンパニー Apparatus and system for swing adsorption process
CN107464944B (en) 2016-05-27 2021-02-02 通用电气公司 Fuel cell system and method of operating the same
BR112018074423A2 (en) 2016-05-31 2019-03-06 Exxonmobil Upstream Research Company apparatus and system for variation adsorption processes
US10427091B2 (en) 2016-05-31 2019-10-01 Exxonmobil Upstream Research Company Apparatus and system for swing adsorption processes
DE102016211214A1 (en) * 2016-06-23 2017-12-28 Trumpf Laser- Und Systemtechnik Gmbh Construction cylinder arrangement for a machine for the layered production of three-dimensional objects, with fiber metal seal
DE102016213846A1 (en) * 2016-07-28 2018-02-01 Robert Bosch Gmbh Temperature control device, battery system, controller and method for heating a battery
CN106299425B (en) * 2016-08-24 2019-02-15 广东工业大学 The removable solid oxide fuel cell power generator of intelligent burner heating
US10434458B2 (en) 2016-08-31 2019-10-08 Exxonmobil Upstream Research Company Apparatus and system for swing adsorption processes related thereto
AU2017320837B2 (en) 2016-09-01 2020-07-23 Exxonmobil Upstream Research Company Swing adsorption processes for removing water using 3A zeolite structures
US10328382B2 (en) 2016-09-29 2019-06-25 Exxonmobil Upstream Research Company Apparatus and system for testing swing adsorption processes
CN110099730A (en) 2016-12-21 2019-08-06 埃克森美孚上游研究公司 Self-supporting structure with foam geometrical form and active material
RU2720940C1 (en) 2016-12-21 2020-05-14 Эксонмобил Апстрим Рисерч Компани Self-supported structures having active materials
US10763533B1 (en) 2017-03-30 2020-09-01 Bloom Energy Corporation Solid oxide fuel cell interconnect having a magnesium containing corrosion barrier layer and method of making thereof
WO2019147516A1 (en) 2018-01-24 2019-08-01 Exxonmobil Upstream Research Company Apparatus and system for temperature swing adsorption
WO2019168628A1 (en) 2018-02-28 2019-09-06 Exxonmobil Upstream Research Company Apparatus and system for swing adsorption processes
US11344640B2 (en) * 2018-04-18 2022-05-31 Anderson Industries, Llc Portable sterilization and decontamination system
US11318410B2 (en) 2018-12-21 2022-05-03 Exxonmobil Upstream Research Company Flow modulation systems, apparatus, and methods for cyclical swing adsorption
US11873836B2 (en) 2019-03-04 2024-01-16 Regal Beloit America, Inc. Blower assembly for gas-burning appliance
US11376545B2 (en) 2019-04-30 2022-07-05 Exxonmobil Upstream Research Company Rapid cycle adsorbent bed
KR102283280B1 (en) * 2019-05-15 2021-07-29 서울과학기술대학교 산학협력단 Fuel cell, fuel cell manufacturing method, and catalyst electrode
US11655910B2 (en) 2019-10-07 2023-05-23 ExxonMobil Technology and Engineering Company Adsorption processes and systems utilizing step lift control of hydraulically actuated poppet valves
WO2021076594A1 (en) 2019-10-16 2021-04-22 Exxonmobil Upstream Research Company Dehydration processes utilizing cationic zeolite rho
DE102020206225A1 (en) 2020-05-18 2021-11-18 Robert Bosch Gesellschaft mit beschränkter Haftung Process for the manufacture of an electrochemical cell
CN111714975B (en) * 2020-06-10 2021-11-23 浙江工业大学 Plate type air inlet purifier, air inlet system and method of vehicle-mounted fuel cell
JP2022022555A (en) * 2020-06-26 2022-02-07 岩谷産業株式会社 Solid oxide fuel cell power generator
CN112086659A (en) * 2020-08-25 2020-12-15 北京理工大学 Fuel cell stack convenient for temperature control
KR102397331B1 (en) * 2021-12-10 2022-05-12 서울대학교산학협력단 Fuel cell system supplied with oxygen enriched air using pressure and temperature swing adsorption technology
KR102374157B1 (en) * 2021-12-15 2022-03-11 서울대학교산학협력단 Fuel cell system supplied with oxygen enriched air using pressure and temperature swing adsorption technology

Citations (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4898792A (en) * 1988-12-07 1990-02-06 Westinghouse Electric Corp. Electrochemical generator apparatus containing modified high temperature insulation and coated surfaces for use with hydrocarbon fuels
US4983471A (en) * 1989-12-28 1991-01-08 Westinghouse Electric Corp. Electrochemical cell apparatus having axially distributed entry of a fuel-spent fuel mixture transverse to the cell lengths
US5047299A (en) * 1990-07-25 1991-09-10 Westinghouse Electric Corp. Electrochemical cell apparatus having an integrated reformer-mixer nozzle-mixer diffuser
US5143800A (en) * 1990-07-25 1992-09-01 Westinghouse Electric Corp. Electrochemical cell apparatus having combusted exhaust gas heat exchange and valving to control the reformable feed fuel composition
US5169730A (en) * 1990-07-25 1992-12-08 Westinghouse Electric Corp. Electrochemical cell apparatus having an exterior fuel mixer nozzle
US5170124A (en) * 1990-06-08 1992-12-08 Minister Of National Defence Of Her Majesty's Canadian Government Method and apparatus for monitoring fuel cell performance
US5302470A (en) * 1989-05-16 1994-04-12 Osaka Gas Co., Ltd. Fuel cell power generation system
US5441821A (en) * 1994-12-23 1995-08-15 Ballard Power Systems Inc. Electrochemical fuel cell system with a regulated vacuum ejector for recirculation of the fluid fuel stream
US5498487A (en) * 1994-08-11 1996-03-12 Westinghouse Electric Corporation Oxygen sensor for monitoring gas mixtures containing hydrocarbons
US5573867A (en) * 1996-01-31 1996-11-12 Westinghouse Electric Corporation Purge gas protected transportable pressurized fuel cell modules and their operation in a power plant
US5601937A (en) * 1995-01-25 1997-02-11 Westinghouse Electric Corporation Hydrocarbon reformer for electrochemical cells
US5733675A (en) * 1995-08-23 1998-03-31 Westinghouse Electric Corporation Electrochemical fuel cell generator having an internal and leak tight hydrocarbon fuel reformer
US5741605A (en) * 1996-03-08 1998-04-21 Westinghouse Electric Corporation Solid oxide fuel cell generator with removable modular fuel cell stack configurations
US6013385A (en) * 1997-07-25 2000-01-11 Emprise Corporation Fuel cell gas management system
US6106964A (en) * 1997-06-30 2000-08-22 Ballard Power Systems Inc. Solid polymer fuel cell system and method for humidifying and adjusting the temperature of a reactant stream
US6280865B1 (en) * 1999-09-24 2001-08-28 Plug Power Inc. Fuel cell system with hydrogen purification subsystem
US6329090B1 (en) * 1999-09-03 2001-12-11 Plug Power Llc Enthalpy recovery fuel cell system
US20020015867A1 (en) * 2000-07-28 2002-02-07 Joe Cargnelli Method and apparatus for humidification and temperature control of incoming fuel cell process gas
US6403245B1 (en) * 1999-05-21 2002-06-11 Microcoating Technologies, Inc. Materials and processes for providing fuel cells and active membranes

Family Cites Families (96)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4575407A (en) * 1962-12-03 1986-03-11 Diller Isaac M Product and process for the activation of an electrolytic cell
DE1809878A1 (en) * 1968-11-20 1970-06-11 Bbc Brown Boveri & Cie Battery with fuel cells made from a solid electrolyte
DE2723947A1 (en) * 1977-05-27 1978-11-30 Varta Batterie ELECTRODE PLATE FOR LEAD ACCUMULATORS
CA1117589A (en) 1978-03-04 1982-02-02 David E. Brown Method of stabilising electrodes coated with mixed oxide electrocatalysts during use in electrochemical cells
DE3112079C2 (en) * 1981-03-27 1983-02-03 Triumph-Adler Aktiengesellschaft für Büro- und Informationstechnik, 8500 Nürnberg Device for lifting the printhead from the platen
US4510756A (en) 1981-11-20 1985-04-16 Consolidated Natural Gas Service Company, Inc. Cogeneration
US4627860A (en) * 1982-07-09 1986-12-09 Hudson Oxygen Therapy Sales Company Oxygen concentrator and test apparatus
FR2539854A1 (en) 1983-04-22 1984-07-27 Cetiat ADSORPTION REFRIGERATION FACILITY ON SOLID ADSORBENT AND METHOD FOR ITS IMPLEMENTATION
US4925745A (en) * 1985-03-29 1990-05-15 Institute Of Gas Technoloy Sulfur tolerant molten carbonate fuel cell anode and process
US4610148A (en) 1985-05-03 1986-09-09 Shelton Samuel V Solid adsorbent heat pump system
US4792502A (en) * 1986-11-14 1988-12-20 International Fuel Cells Corporation Apparatus for producing nitrogen
US4913982A (en) * 1986-12-15 1990-04-03 Allied-Signal Inc. Fabrication of a monolithic solid oxide fuel cell
US4847173A (en) * 1987-01-21 1989-07-11 Mitsubishi Denki Kabushiki Kaisha Electrode for fuel cell
US4804592A (en) * 1987-10-16 1989-02-14 The United States Of America As Represented By The United States Department Of Energy Composite electrode for use in electrochemical cells
DE3932217A1 (en) 1989-04-25 1990-10-31 Linde Ag METHOD FOR OPERATING HIGH-TEMPERATURE FUEL CELLS
US5290642A (en) * 1990-09-11 1994-03-01 Alliedsignal Aerospace Method of fabricating a monolithic solid oxide fuel cell
US5162167A (en) * 1990-09-11 1992-11-10 Allied-Signal Inc. Apparatus and method of fabricating a monolithic solid oxide fuel cell
US5256499A (en) * 1990-11-13 1993-10-26 Allied Signal Aerospace Monolithic solid oxide fuel cells with integral manifolds
US5248712A (en) * 1990-12-21 1993-09-28 Takeda Chemical Industries, Ltd. Binders for forming a ceramics sheet and applications thereof
US5382315A (en) * 1991-02-11 1995-01-17 Microelectronics And Computer Technology Corporation Method of forming etch mask using particle beam deposition
JPH04292865A (en) * 1991-03-20 1992-10-16 Ngk Insulators Ltd Solid electrolytic fuel cell
US5215946A (en) * 1991-08-05 1993-06-01 Allied-Signal, Inc. Preparation of powder articles having improved green strength
JPH06101932A (en) 1992-08-27 1994-04-12 Hitachi Ltd Absorptive heat pump and cogeneration system using exhaust heat
US5273837A (en) * 1992-12-23 1993-12-28 Corning Incorporated Solid electrolyte fuel cells
JP3145522B2 (en) 1993-01-18 2001-03-12 三菱重工業株式会社 Solid oxide fuel cell
US5368667A (en) * 1993-01-29 1994-11-29 Alliedsignal Inc. Preparation of devices that include a thin ceramic layer
JP3267034B2 (en) * 1993-03-10 2002-03-18 株式会社村田製作所 Method for manufacturing solid oxide fuel cell
US5342705A (en) * 1993-06-04 1994-08-30 Allied-Signal, Inc. Monolithic fuel cell having a multilayer interconnect
US5678410A (en) 1993-08-06 1997-10-21 Toyota Jidosha Kabushiki Kaisha Combined system of fuel cell and air-conditioning apparatus
JP3064167B2 (en) * 1993-09-01 2000-07-12 三菱重工業株式会社 Solid electrolyte fuel cell
US5589285A (en) * 1993-09-09 1996-12-31 Technology Management, Inc. Electrochemical apparatus and process
TW299345B (en) 1994-02-18 1997-03-01 Westinghouse Electric Corp
JP3349245B2 (en) * 1994-03-04 2002-11-20 三菱重工業株式会社 Method for manufacturing solid oxide fuel cell
US5948221A (en) * 1994-08-08 1999-09-07 Ztek Corporation Pressurized, integrated electrochemical converter energy system
US6001761A (en) * 1994-09-27 1999-12-14 Nippon Shokubai Co., Ltd. Ceramics sheet and production method for same
DK112994A (en) * 1994-09-29 1996-03-30 Haldor Topsoe As Process for producing electricity in an internal reformed high temperature fuel cell
EP0857702B1 (en) * 1994-11-09 2000-08-23 Ngk Insulators, Ltd. Method for producing ceramic substrate
US5505824A (en) * 1995-01-06 1996-04-09 United Technologies Corporation Propellant generator and method of generating propellants
US5641585A (en) 1995-03-21 1997-06-24 Lockheed Idaho Technologies Company Miniature ceramic fuel cell
US5925322A (en) * 1995-10-26 1999-07-20 H Power Corporation Fuel cell or a partial oxidation reactor or a heat engine and an oxygen-enriching device and method therefor
JPH09199143A (en) 1996-01-19 1997-07-31 Murata Mfg Co Ltd Manufacture of solid-electrolyte fuel cell
JPH09223506A (en) * 1996-02-14 1997-08-26 Murata Mfg Co Ltd Manufacture of solid electrolyte fuel cell
JPH09245811A (en) * 1996-03-12 1997-09-19 Murata Mfg Co Ltd Manufacture of solid electrolyte fuel cell
JPH09245810A (en) * 1996-03-12 1997-09-19 Murata Mfg Co Ltd Manufacture of solid electrolyte fuel cell
JPH09277226A (en) * 1996-04-15 1997-10-28 Murata Mfg Co Ltd Manufacture of solid electrolyte type fuel cell
US6054229A (en) 1996-07-19 2000-04-25 Ztek Corporation System for electric generation, heating, cooling, and ventilation
EP0823742A1 (en) 1996-08-08 1998-02-11 Sulzer Innotec Ag Plant for the simultaneous production of electric and thermal energy
US5686196A (en) * 1996-10-09 1997-11-11 Westinghouse Electric Corporation System for operating solid oxide fuel cell generator on diesel fuel
US5955039A (en) * 1996-12-19 1999-09-21 Siemens Westinghouse Power Corporation Coal gasification and hydrogen production system and method
US6238816B1 (en) * 1996-12-30 2001-05-29 Technology Management, Inc. Method for steam reforming hydrocarbons using a sulfur-tolerant catalyst
US5768904A (en) 1997-05-02 1998-06-23 Uop Llc Processes for integrating a continuous sorption cooling process with an external process
JP3988206B2 (en) * 1997-05-15 2007-10-10 トヨタ自動車株式会社 Fuel cell device
US6032402A (en) * 1997-05-20 2000-03-07 Wright & Mcgill Co. Fish hook and weed guard device
DE59807606D1 (en) * 1997-06-10 2003-04-30 Goldschmidt Ag Th Foamable metal body
AUPO724997A0 (en) * 1997-06-10 1997-07-03 Ceramic Fuel Cells Limited A fuel cell assembly
US5922488A (en) * 1997-08-15 1999-07-13 Exxon Research And Engineering Co., Co-tolerant fuel cell electrode
JP3456378B2 (en) * 1997-08-21 2003-10-14 株式会社村田製作所 Solid oxide fuel cell
US6921597B2 (en) * 1998-09-14 2005-07-26 Questair Technologies Inc. Electrical current generation system
JP2000281438A (en) * 1999-03-31 2000-10-10 Nippon Shokubai Co Ltd Zirconia sheet and its production
US6302402B1 (en) 1999-07-07 2001-10-16 Air Products And Chemicals, Inc. Compliant high temperature seals for dissimilar materials
US6280869B1 (en) * 1999-07-29 2001-08-28 Nexant, Inc. Fuel cell stack system and operating method
US6605316B1 (en) * 1999-07-31 2003-08-12 The Regents Of The University Of California Structures and fabrication techniques for solid state electrochemical devices
JP2001068127A (en) 1999-08-30 2001-03-16 Toyota Autom Loom Works Ltd Fuel cell cooling device and fuel cell system
US6489050B1 (en) * 1999-11-01 2002-12-03 Technology Management, Inc. Apparatus and method for cooling high-temperature fuel cell stacks
US6361892B1 (en) * 1999-12-06 2002-03-26 Technology Management, Inc. Electrochemical apparatus with reactant micro-channels
EP1113518B1 (en) * 1999-12-27 2013-07-10 Corning Incorporated Solid oxide electrolyte, fuel cell module and manufacturing method
US6451466B1 (en) * 2000-04-06 2002-09-17 Utc Fuel Cells, Llc Functional integration of multiple components for a fuel cell power plant
US6630264B2 (en) * 2000-05-01 2003-10-07 Delphi Technologies, Inc. Solid oxide fuel cell process gas sampling for analysis
US6835488B2 (en) * 2000-05-08 2004-12-28 Honda Giken Kogyo Kabushiki Kaisha Fuel cell with patterned electrolyte/electrode interface
AU2001274926A1 (en) * 2000-05-22 2001-12-03 Acumentrics Corporation Electrode-supported solid state electrochemical cell
US6723459B2 (en) 2000-07-12 2004-04-20 Sulzer Hexis Ag Plant with high temperature fuel cells
ATE462202T1 (en) * 2000-08-18 2010-04-15 Versa Power Systems Ltd HIGH TEMPERATURE RESISTANT GAS SEALS
AU2001289446A1 (en) * 2000-09-01 2002-03-13 Fuelcell Energy, Ltd. Anode oxidation protection in a high-temperature fuel cell
US7097925B2 (en) * 2000-10-30 2006-08-29 Questair Technologies Inc. High temperature fuel cell power plant
CA2424728A1 (en) * 2000-11-08 2002-05-16 Global Thermoelectric Inc. Fuel cell interconnect
US6811913B2 (en) * 2000-11-15 2004-11-02 Technology Management, Inc. Multipurpose reversible electrochemical system
US20020142198A1 (en) * 2000-12-08 2002-10-03 Towler Gavin P. Process for air enrichment in producing hydrogen for use with fuel cells
WO2002056399A2 (en) * 2001-01-12 2002-07-18 Global Thermoelectric Inc. Redox solid oxide fuel cell
AU2002241913A1 (en) 2001-01-17 2002-07-30 Engen Group, Inc. Stationary energy center
US7294421B2 (en) * 2001-02-07 2007-11-13 Delphi Technologies, Inc. Solid oxide auxiliary power unit reformate control
CA2439586C (en) * 2001-03-02 2012-02-28 Mesosystems Technology, Inc. Ammonia-based hydrogen generation apparatus and method for using same
US6677070B2 (en) * 2001-04-19 2004-01-13 Hewlett-Packard Development Company, L.P. Hybrid thin film/thick film solid oxide fuel cell and method of manufacturing the same
US6692859B2 (en) * 2001-05-09 2004-02-17 Delphi Technologies, Inc. Fuel and air supply base manifold for modular solid oxide fuel cells
US6623880B1 (en) * 2001-05-29 2003-09-23 The United States Of America As Represented By The Department Of Energy Fuel cell-fuel cell hybrid system
US6635375B1 (en) * 2001-05-29 2003-10-21 The United States Of America As Represented By The United States Department Of Energy Planar solid oxide fuel cell with staged indirect-internal air and fuel preheating and reformation
JP2003083634A (en) 2001-09-06 2003-03-19 Sekisui Chem Co Ltd Heat pump system
US6740441B2 (en) * 2001-12-18 2004-05-25 The Regents Of The University Of California Metal current collect protected by oxide film
US7067208B2 (en) * 2002-02-20 2006-06-27 Ion America Corporation Load matched power generation system including a solid oxide fuel cell and a heat pump and an optional turbine
US20030196893A1 (en) * 2002-04-23 2003-10-23 Mcelroy James Frederick High-temperature low-hydration ion exchange membrane electrochemical cell
US20030215689A1 (en) * 2002-05-16 2003-11-20 Keegan Kevin R. Solid oxide fuel cell with a metal foam seal
US6821663B2 (en) * 2002-10-23 2004-11-23 Ion America Corporation Solid oxide regenerative fuel cell
US7045238B2 (en) * 2003-03-24 2006-05-16 Ion America Corporation SORFC power and oxygen generation method and system
US6924053B2 (en) * 2003-03-24 2005-08-02 Ion America Corporation Solid oxide regenerative fuel cell with selective anode tail gas circulation
US7482078B2 (en) * 2003-04-09 2009-01-27 Bloom Energy Corporation Co-production of hydrogen and electricity in a high temperature electrochemical system
US7364810B2 (en) * 2003-09-03 2008-04-29 Bloom Energy Corporation Combined energy storage and fuel generation with reversible fuel cells
US7575822B2 (en) * 2003-04-09 2009-08-18 Bloom Energy Corporation Method of optimizing operating efficiency of fuel cells

Patent Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4898792A (en) * 1988-12-07 1990-02-06 Westinghouse Electric Corp. Electrochemical generator apparatus containing modified high temperature insulation and coated surfaces for use with hydrocarbon fuels
US5302470A (en) * 1989-05-16 1994-04-12 Osaka Gas Co., Ltd. Fuel cell power generation system
US4983471A (en) * 1989-12-28 1991-01-08 Westinghouse Electric Corp. Electrochemical cell apparatus having axially distributed entry of a fuel-spent fuel mixture transverse to the cell lengths
US5170124A (en) * 1990-06-08 1992-12-08 Minister Of National Defence Of Her Majesty's Canadian Government Method and apparatus for monitoring fuel cell performance
US5047299A (en) * 1990-07-25 1991-09-10 Westinghouse Electric Corp. Electrochemical cell apparatus having an integrated reformer-mixer nozzle-mixer diffuser
US5143800A (en) * 1990-07-25 1992-09-01 Westinghouse Electric Corp. Electrochemical cell apparatus having combusted exhaust gas heat exchange and valving to control the reformable feed fuel composition
US5169730A (en) * 1990-07-25 1992-12-08 Westinghouse Electric Corp. Electrochemical cell apparatus having an exterior fuel mixer nozzle
US5498487A (en) * 1994-08-11 1996-03-12 Westinghouse Electric Corporation Oxygen sensor for monitoring gas mixtures containing hydrocarbons
US5441821A (en) * 1994-12-23 1995-08-15 Ballard Power Systems Inc. Electrochemical fuel cell system with a regulated vacuum ejector for recirculation of the fluid fuel stream
US5601937A (en) * 1995-01-25 1997-02-11 Westinghouse Electric Corporation Hydrocarbon reformer for electrochemical cells
US5733675A (en) * 1995-08-23 1998-03-31 Westinghouse Electric Corporation Electrochemical fuel cell generator having an internal and leak tight hydrocarbon fuel reformer
US5573867A (en) * 1996-01-31 1996-11-12 Westinghouse Electric Corporation Purge gas protected transportable pressurized fuel cell modules and their operation in a power plant
US5741605A (en) * 1996-03-08 1998-04-21 Westinghouse Electric Corporation Solid oxide fuel cell generator with removable modular fuel cell stack configurations
US6106964A (en) * 1997-06-30 2000-08-22 Ballard Power Systems Inc. Solid polymer fuel cell system and method for humidifying and adjusting the temperature of a reactant stream
US6013385A (en) * 1997-07-25 2000-01-11 Emprise Corporation Fuel cell gas management system
US6436562B1 (en) * 1997-07-25 2002-08-20 Emprise Technology Associates Corp. Fuel-cell engine stream conditioning system
US6403245B1 (en) * 1999-05-21 2002-06-11 Microcoating Technologies, Inc. Materials and processes for providing fuel cells and active membranes
US6329090B1 (en) * 1999-09-03 2001-12-11 Plug Power Llc Enthalpy recovery fuel cell system
US6280865B1 (en) * 1999-09-24 2001-08-28 Plug Power Inc. Fuel cell system with hydrogen purification subsystem
US20020015867A1 (en) * 2000-07-28 2002-02-07 Joe Cargnelli Method and apparatus for humidification and temperature control of incoming fuel cell process gas

Cited By (163)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7255956B2 (en) 2002-02-20 2007-08-14 Bloom Energy Corporation Environmentally tolerant anode catalyst for a solid oxide fuel cell
US20030165732A1 (en) * 2002-02-20 2003-09-04 Ion America Corporation Environmentally tolerant anode catalyst for a solid oxide fuel cell
US20060204798A1 (en) * 2003-03-24 2006-09-14 Ion America Corporation SORFC power and oxygen generation method and system
US20040191598A1 (en) * 2003-03-24 2004-09-30 Ion America Corporation SORFC power and oxygen generation method and system
US6924053B2 (en) 2003-03-24 2005-08-02 Ion America Corporation Solid oxide regenerative fuel cell with selective anode tail gas circulation
US20050214609A1 (en) * 2003-03-24 2005-09-29 Ion America Corporation Solid oxide fuel cell with selective anode tail gas circulation
US7572530B2 (en) 2003-03-24 2009-08-11 Bloom Energy Corporation SORFC power and oxygen generation method and system
US7045238B2 (en) 2003-03-24 2006-05-16 Ion America Corporation SORFC power and oxygen generation method and system
US7575822B2 (en) 2003-04-09 2009-08-18 Bloom Energy Corporation Method of optimizing operating efficiency of fuel cells
US8663859B2 (en) 2003-04-09 2014-03-04 Bloom Energy Corporation Method of optimizing operating efficiency of fuel cells
US20070196702A1 (en) * 2003-04-09 2007-08-23 Bloom Energy Corporation Low pressure hydrogen fueled vehicle and method of operating same
US8277992B2 (en) 2003-04-09 2012-10-02 Bloom Energy Corporation Method of optimizing operating efficiency of fuel cells
US8071246B2 (en) 2003-04-09 2011-12-06 Bloom Energy Corporation Method of optimizing operating efficiency of fuel cells
US8071241B2 (en) * 2003-04-09 2011-12-06 Bloom Energy Corporation Method for the co-production of hydrogen and electricity in a high temperature electrochemical system
US7878280B2 (en) 2003-04-09 2011-02-01 Bloom Energy Corporation Low pressure hydrogen fueled vehicle and method of operating same
US20110011362A1 (en) * 2003-04-09 2011-01-20 Bloom Energy Corporation Low pressure hydrogen fueled vehicle and method of operating same
US20080318092A1 (en) * 2003-04-09 2008-12-25 Bloom Energy Corporation Co-production of hydrogen and electricity in a high temperature electrochemical system
US7482078B2 (en) 2003-04-09 2009-01-27 Bloom Energy Corporation Co-production of hydrogen and electricity in a high temperature electrochemical system
US7364810B2 (en) 2003-09-03 2008-04-29 Bloom Energy Corporation Combined energy storage and fuel generation with reversible fuel cells
US7781112B2 (en) 2003-09-03 2010-08-24 Bloom Energy Corporation Combined energy storage and fuel generation with reversible fuel cells
US7306641B2 (en) * 2003-09-12 2007-12-11 Hewlett-Packard Development Company, L.P. Integral fuel cartridge and filter
US9401524B2 (en) 2003-09-29 2016-07-26 Ballard Power Systems Inc. Compliant stack for a planar solid oxide fuel cell
US20060210858A1 (en) * 2003-09-29 2006-09-21 Warrier Sunil G Compliant stack for a planar solid oxide fuel cell
US20050136299A1 (en) * 2003-12-17 2005-06-23 Richey Joseph B.Ii Oxygen supply system
US7704618B2 (en) 2004-01-22 2010-04-27 Bloom Energy Corporation High temperature fuel cell system and method of operating same
US7422810B2 (en) 2004-01-22 2008-09-09 Bloom Energy Corporation High temperature fuel cell system and method of operating same
US20050164051A1 (en) * 2004-01-22 2005-07-28 Ion America Corporation High temperature fuel cell system and method of operating same
US20110189567A1 (en) * 2004-01-22 2011-08-04 Bloom Energy Corporation High Temperature Fuel Cell System and Method of Operating the Same
US7901814B2 (en) 2004-01-22 2011-03-08 Bloom Energy Corporation High temperature fuel cell system and method of operating same
US20080311445A1 (en) * 2004-01-22 2008-12-18 Bloom Energy Corporation High temperature fuel cell system and method of operating same
US20100203417A1 (en) * 2004-01-22 2010-08-12 Bloom Energy Corporation High temperature fuel cell system and method of operating same
US20060040168A1 (en) * 2004-08-20 2006-02-23 Ion America Corporation Nanostructured fuel cell electrode
US7524572B2 (en) 2005-04-07 2009-04-28 Bloom Energy Corporation Fuel cell system with thermally integrated combustor and corrugated foil reformer
US20060228598A1 (en) * 2005-04-07 2006-10-12 Swaminathan Venkataraman Fuel cell system with thermally integrated combustor and corrugated foil reformer
US20060240296A1 (en) * 2005-04-20 2006-10-26 Grieve Malcolm J Regenerable method and system for desulfurizing reformate
US7931707B2 (en) * 2005-04-20 2011-04-26 Delphi Technologies, Inc. Regenerable method and system for desulfurizing reformate
US8691462B2 (en) 2005-05-09 2014-04-08 Modine Manufacturing Company High temperature fuel cell system with integrated heat exchanger network
US20060251939A1 (en) * 2005-05-09 2006-11-09 Bandhauer Todd M High temperature fuel cell system with integrated heat exchanger network
US20060251940A1 (en) * 2005-05-09 2006-11-09 Bandhauer Todd M High temperature fuel cell system with integrated heat exchanger network
US9413017B2 (en) 2005-05-09 2016-08-09 Bloom Energy Corporation High temperature fuel cell system with integrated heat exchanger network
US20060251934A1 (en) * 2005-05-09 2006-11-09 Ion America Corporation High temperature fuel cell system with integrated heat exchanger network
US7858256B2 (en) 2005-05-09 2010-12-28 Bloom Energy Corporation High temperature fuel cell system with integrated heat exchanger network
US20100081018A1 (en) * 2005-05-10 2010-04-01 Bloom Energy Corporation Increasing thermal dissipation of fuel cell stacks under partial electrical load
US9166246B2 (en) 2005-05-10 2015-10-20 Bloom Energy Corporation Increasing thermal dissipation of fuel cell stacks under partial electrical load
US8685579B2 (en) 2005-05-10 2014-04-01 Bloom Enery Corporation Increasing thermal dissipation of fuel cell stacks under partial electrical load
US20060257696A1 (en) * 2005-05-10 2006-11-16 Ion America Corporation Increasing thermal dissipation of fuel cell stacks under partial electrical load
US7700210B2 (en) 2005-05-10 2010-04-20 Bloom Energy Corporation Increasing thermal dissipation of fuel cell stacks under partial electrical load
US20070017367A1 (en) * 2005-07-25 2007-01-25 Ion America Corporation Partial pressure swing adsorption system for providing hydrogen to a vehicle fuel cell
US7591880B2 (en) 2005-07-25 2009-09-22 Bloom Energy Corporation Fuel cell anode exhaust fuel recovery by adsorption
US20100239924A1 (en) * 2005-07-25 2010-09-23 Ion America Corporation Fuel cell system with partial recycling of anode exhaust
US8101307B2 (en) 2005-07-25 2012-01-24 Bloom Energy Corporation Fuel cell system with electrochemical anode exhaust recycling
US20070017368A1 (en) * 2005-07-25 2007-01-25 Ion America Corporation Gas separation method and apparatus using partial pressure swing adsorption
US9911989B2 (en) 2005-07-25 2018-03-06 Bloom Energy Corporation Fuel cell system with partial recycling of anode exhaust
US20070017369A1 (en) * 2005-07-25 2007-01-25 Ion America Corporation Fuel cell anode exhaust fuel recovery by adsorption
US20070178338A1 (en) * 2005-07-25 2007-08-02 Ion America Corporation Fuel cell system with electrochemical anode exhaust recycling
US7520916B2 (en) 2005-07-25 2009-04-21 Bloom Energy Corporation Partial pressure swing adsorption system for providing hydrogen to a vehicle fuel cell
US9947955B2 (en) 2006-01-23 2018-04-17 Bloom Energy Corporation Modular fuel cell system
US9190693B2 (en) 2006-01-23 2015-11-17 Bloom Energy Corporation Modular fuel cell system
US20070238007A1 (en) * 2006-03-30 2007-10-11 Shinko Electric Industries Co., Ltd. Solid electrolyte fuel cell and process for the production thereof
US8304129B2 (en) * 2006-03-30 2012-11-06 Shinko Electric Industries Co., Ltd. Solid electrolyte fuel cell including a first cathode layer and a second cathode layer
US8057944B2 (en) 2006-04-03 2011-11-15 Bloom Energy Corporation Hybrid reformer for fuel flexibility
US20100203416A1 (en) * 2006-04-03 2010-08-12 Bloom Energy Corporation Hybrid reformer for fuel flexibility
US20070231635A1 (en) * 2006-04-03 2007-10-04 Bloom Energy Corporation Fuel cell system operated on liquid fuels
US20070231631A1 (en) * 2006-04-03 2007-10-04 Bloom Energy Corporation Hybrid reformer for fuel flexibility
US7704617B2 (en) 2006-04-03 2010-04-27 Bloom Energy Corporation Hybrid reformer for fuel flexibility
US8822094B2 (en) 2006-04-03 2014-09-02 Bloom Energy Corporation Fuel cell system operated on liquid fuels
US20070259225A1 (en) * 2006-04-21 2007-11-08 Michael Penev Recovering a reactant from a fuel cell exhaust flow
US8158290B2 (en) * 2006-04-21 2012-04-17 Plug Power, Inc. Recovering a reactant from a fuel cell exhaust flow
US8026013B2 (en) 2006-08-14 2011-09-27 Modine Manufacturing Company Annular or ring shaped fuel cell unit
US7659022B2 (en) 2006-08-14 2010-02-09 Modine Manufacturing Company Integrated solid oxide fuel cell and fuel processor
US8241801B2 (en) 2006-08-14 2012-08-14 Modine Manufacturing Company Integrated solid oxide fuel cell and fuel processor
US20080057359A1 (en) * 2006-09-06 2008-03-06 Bloom Energy Corporation Flexible fuel cell system configuration to handle multiple fuels
US7968245B2 (en) 2006-09-25 2011-06-28 Bloom Energy Corporation High utilization stack
US20080076006A1 (en) * 2006-09-25 2008-03-27 Ion America Corporation High utilization stack
US10622642B2 (en) 2006-10-18 2020-04-14 Bloom Energy Corporation Anode with remarkable stability under conditions of extreme fuel starvation
US8748056B2 (en) 2006-10-18 2014-06-10 Bloom Energy Corporation Anode with remarkable stability under conditions of extreme fuel starvation
US10615444B2 (en) 2006-10-18 2020-04-07 Bloom Energy Corporation Anode with high redox stability
US20080096080A1 (en) * 2006-10-18 2008-04-24 Bloom Energy Corporation Anode with remarkable stability under conditions of extreme fuel starvation
US9812714B2 (en) 2006-10-18 2017-11-07 Bloom Energy Corporation Anode with remarkable stability under conditions of extreme fuel starvation
US20080096073A1 (en) * 2006-10-23 2008-04-24 Bloom Energy Corporation Dual function heat exchanger for start-up humidification and facility heating in SOFC system
US8435689B2 (en) 2006-10-23 2013-05-07 Bloom Energy Corporation Dual function heat exchanger for start-up humidification and facility heating in SOFC system
US7393603B1 (en) 2006-12-20 2008-07-01 Bloom Energy Corporation Methods for fuel cell system optimization
US20080152959A1 (en) * 2006-12-20 2008-06-26 Bloom Energy Corporation Methods for fuel cell system optimization
US7833668B2 (en) 2007-03-30 2010-11-16 Bloom Energy Corporation Fuel cell system with greater than 95% fuel utilization
US7883803B2 (en) 2007-03-30 2011-02-08 Bloom Energy Corporation SOFC system producing reduced atmospheric carbon dioxide using a molten carbonated carbon dioxide pump
US20080241612A1 (en) * 2007-03-30 2008-10-02 Bloom Energy Corporation Fuel cell system with one hundred percent fuel utilization
US20080241638A1 (en) * 2007-03-30 2008-10-02 Bloom Energy Corporation SOFC system producing reduced atmospheric carbon dioxide using a molten carbonated carbon dioxide pump
US20080254336A1 (en) * 2007-04-13 2008-10-16 Bloom Energy Corporation Composite anode showing low performance loss with time
US20080261099A1 (en) * 2007-04-13 2008-10-23 Bloom Energy Corporation Heterogeneous ceramic composite SOFC electrolyte
US10593981B2 (en) 2007-04-13 2020-03-17 Bloom Energy Corporation Heterogeneous ceramic composite SOFC electrolyte
US7846599B2 (en) 2007-06-04 2010-12-07 Bloom Energy Corporation Method for high temperature fuel cell system start up and shutdown
US8137855B2 (en) 2007-07-26 2012-03-20 Bloom Energy Corporation Hot box design with a multi-stream heat exchanger and single air control
US8920997B2 (en) 2007-07-26 2014-12-30 Bloom Energy Corporation Hybrid fuel heat exchanger—pre-reformer in SOFC systems
US9166240B2 (en) 2007-07-26 2015-10-20 Bloom Energy Corporation Hot box design with a multi-stream heat exchanger and single air control
US9680175B2 (en) 2007-07-26 2017-06-13 Bloom Energy Corporation Integrated fuel line to support CPOX and SMR reactions in SOFC systems
US9722273B2 (en) 2007-08-15 2017-08-01 Bloom Energy Corporation Fuel cell system components
US8852820B2 (en) 2007-08-15 2014-10-07 Bloom Energy Corporation Fuel cell stack module shell with integrated heat exchanger
US8333919B2 (en) 2007-11-13 2012-12-18 Bloom Energy Corporation Electrolyte supported cell designed for longer life and higher power
US8999601B2 (en) 2007-11-13 2015-04-07 Bloom Energy Corporation Electrolyte supported cell designed for longer life and higher power
US8067129B2 (en) 2007-11-13 2011-11-29 Bloom Energy Corporation Electrolyte supported cell designed for longer life and higher power
US9991540B2 (en) 2007-11-13 2018-06-05 Bloom Energy Corporation Electrolyte supported cell designed for longer life and higher power
US9246184B1 (en) 2007-11-13 2016-01-26 Bloom Energy Corporation Electrolyte supported cell designed for longer life and higher power
US8288041B2 (en) 2008-02-19 2012-10-16 Bloom Energy Corporation Fuel cell system containing anode tail gas oxidizer and hybrid heat exchanger/reformer
US8535839B2 (en) 2008-02-19 2013-09-17 Bloom Energy Corporation Fuel cell system containing anode tail gas oxidizer and hybrid heat exchanger/reformer
US9105894B2 (en) 2008-02-19 2015-08-11 Bloom Energy Corporation Fuel cell system containing anode tail gas oxidizer and hybrid heat exchanger/reformer
US20090208784A1 (en) * 2008-02-19 2009-08-20 Bloom Energy Corporation Fuel cell system containing anode tail gas oxidizer and hybrid heat exchanger/reformer
US20090208785A1 (en) * 2008-02-20 2009-08-20 Bloom Energy Cororation SOFC electrochemical anode tail gas oxidizer
US8968958B2 (en) 2008-07-08 2015-03-03 Bloom Energy Corporation Voltage lead jumper connected fuel cell columns
US9287571B2 (en) 2008-07-23 2016-03-15 Bloom Energy Corporation Operation of fuel cell systems with reduced carbon formation and anode leading edge damage
US20100047637A1 (en) * 2008-07-23 2010-02-25 Bloom Energy Corporation Operation of fuel cell systems with reduced carbon formation and anode leading edge damage
US20100028736A1 (en) * 2008-08-01 2010-02-04 Georgia Tech Research Corporation Hybrid Ionomer Electrochemical Devices
US20110171544A1 (en) * 2008-09-19 2011-07-14 Mtu Onsite Energy Gmbh Fuel cell assembly with improved gas recirculation
US20100107435A1 (en) * 2008-10-31 2010-05-06 Jacob George Methods and Apparatus for Drying Ceramic Green Bodies with Microwaves
US8020314B2 (en) * 2008-10-31 2011-09-20 Corning Incorporated Methods and apparatus for drying ceramic green bodies with microwaves
US8409760B2 (en) 2009-01-20 2013-04-02 Adaptive Materials, Inc. Method for controlling a water based fuel reformer
US20100183930A1 (en) * 2009-01-20 2010-07-22 Adaptive Materials, Inc. Method for controlling a water based fuel reformer
US8936888B2 (en) 2009-01-30 2015-01-20 Adaptive Materials, Inc. Fuel cell system with flame protection member
US20110189572A1 (en) * 2009-01-30 2011-08-04 Adaptive Materials, Inc. Fuel cell system with flame protection member
US8617763B2 (en) 2009-08-12 2013-12-31 Bloom Energy Corporation Internal reforming anode for solid oxide fuel cells
US20110039183A1 (en) * 2009-08-12 2011-02-17 Bloom Energy Corporation Internal reforming anode for solid oxide fuel cells
US20110053027A1 (en) * 2009-09-02 2011-03-03 Bloom Energy Corporation Multi-Stream Heat Exchanger for a Fuel Cell System
US8445156B2 (en) 2009-09-02 2013-05-21 Bloom Energy Corporation Multi-stream heat exchanger for a fuel cell system
US9401517B2 (en) 2009-09-02 2016-07-26 Bloom Energy Corporation Multi-stream heat exchanger for a fuel cell system
US20110183233A1 (en) * 2010-01-26 2011-07-28 Bloom Energy Corporation Phase Stable Doped Zirconia Electrolyte Compositions with Low Degradation
US8580456B2 (en) 2010-01-26 2013-11-12 Bloom Energy Corporation Phase stable doped zirconia electrolyte compositions with low degradation
US9413024B2 (en) 2010-01-26 2016-08-09 Bloom Energy Corporation Phase stable doped zirconia electrolyte compositions with low degradation
US9799909B2 (en) 2010-01-26 2017-10-24 Bloom Energy Corporation Phase stable doped zirconia electrolyte compositions with low degradation
US20110189578A1 (en) * 2010-02-01 2011-08-04 Adaptive Materials, Inc. Fuel cell system including a resilient manifold interconnecting member
US8796888B2 (en) 2010-07-07 2014-08-05 Adaptive Materials, Inc. Wearable power management system
US9190673B2 (en) 2010-09-01 2015-11-17 Bloom Energy Corporation SOFC hot box components
US9520602B2 (en) 2010-09-01 2016-12-13 Bloom Energy Corporation SOFC hot box components
US20120077099A1 (en) * 2010-09-23 2012-03-29 Adaptive Materials, Inc. Solid oxide fuel cell with multiple fuel streams
US10840535B2 (en) 2010-09-24 2020-11-17 Bloom Energy Corporation Fuel cell mechanical components
US8822101B2 (en) 2010-09-24 2014-09-02 Bloom Energy Corporation Fuel cell mechanical components
US8440362B2 (en) 2010-09-24 2013-05-14 Bloom Energy Corporation Fuel cell mechanical components
US8877399B2 (en) 2011-01-06 2014-11-04 Bloom Energy Corporation SOFC hot box components
US9941525B2 (en) 2011-01-06 2018-04-10 Bloom Energy Corporation SOFC hot box components
US10797327B2 (en) 2011-01-06 2020-10-06 Bloom Energy Corporation SOFC hot box components
US9780392B2 (en) 2011-01-06 2017-10-03 Bloom Energy Corporation SOFC hot box components
US8968943B2 (en) 2011-01-06 2015-03-03 Bloom Energy Corporation SOFC hot box components
US9991526B2 (en) 2011-01-06 2018-06-05 Bloom Energy Corporation SOFC hot box components
US8563180B2 (en) 2011-01-06 2013-10-22 Bloom Energy Corporation SOFC hot box components
US20120264029A1 (en) * 2011-04-14 2012-10-18 Hitachi, Ltd. Fuel cell system
US9601792B2 (en) 2011-12-05 2017-03-21 Doosan Heavy Industries & Construction Co., Ltd. Fuel cell system and method for driving same
KR101441489B1 (en) * 2011-12-05 2014-09-18 두산중공업 주식회사 Fuel cell system and driving method thereof
WO2013085216A1 (en) * 2011-12-05 2013-06-13 두산중공업 주식회사 Fuel cell system and method for driving same
US9515344B2 (en) 2012-11-20 2016-12-06 Bloom Energy Corporation Doped scandia stabilized zirconia electrolyte compositions
US10381673B2 (en) 2012-11-20 2019-08-13 Bloom Energy Corporation Doped scandia stabilized zirconia electrolyte compositions
US9755263B2 (en) 2013-03-15 2017-09-05 Bloom Energy Corporation Fuel cell mechanical components
US9799902B2 (en) 2013-10-23 2017-10-24 Bloom Energy Corporation Pre-reformer for selective reformation of higher hydrocarbons
US9287572B2 (en) 2013-10-23 2016-03-15 Bloom Energy Corporation Pre-reformer for selective reformation of higher hydrocarbons
US9461320B2 (en) 2014-02-12 2016-10-04 Bloom Energy Corporation Structure and method for fuel cell system where multiple fuel cells and power electronics feed loads in parallel allowing for integrated electrochemical impedance spectroscopy (EIS)
US9216405B1 (en) * 2014-06-26 2015-12-22 Kraton Polymers U.S. Llc Rotary enthalpy exchange wheel having sulfonated block copolymer
US10651496B2 (en) 2015-03-06 2020-05-12 Bloom Energy Corporation Modular pad for a fuel cell system
US10347930B2 (en) 2015-03-24 2019-07-09 Bloom Energy Corporation Perimeter electrolyte reinforcement layer composition for solid oxide fuel cell electrolytes
US10680251B2 (en) 2017-08-28 2020-06-09 Bloom Energy Corporation SOFC including redox-tolerant anode electrode and system including the same
US11398634B2 (en) 2018-03-27 2022-07-26 Bloom Energy Corporation Solid oxide fuel cell system and method of operating the same using peak shaving gas
US11876257B2 (en) 2018-03-27 2024-01-16 Bloom Energy Corporation Solid oxide fuel cell system and method of operating the same using peak shaving gas
US11616249B2 (en) 2019-03-22 2023-03-28 Bloom Energy Corporation Solid oxide fuel cell system with hydrogen pumping cell with carbon monoxide tolerant anodes and integrated shift reactor
US11322767B2 (en) 2019-04-12 2022-05-03 Bloom Energy Corporation Solid oxide fuel cell system with hydrogen pumping cell with carbon monoxide tolerant anodes and integrated shift reactor
US11777125B2 (en) 2019-04-12 2023-10-03 Bloom Energy Corporation Solid oxide fuel cell system with hydrogen pumping cell with carbon monoxide tolerant anodes and integrated shift reactor
EP4071867A3 (en) * 2021-04-08 2022-11-09 Bloom Energy Corporation Hydrogen pumping proton exchange membrane electrochemical cell with carbon monoxide tolerant anode and method of making thereof
EP4147768A1 (en) * 2021-09-10 2023-03-15 Hamilton Sundstrand Corporation Water recovery system for fuel cells

Also Published As

Publication number Publication date
US20030170527A1 (en) 2003-09-11
WO2003071619A3 (en) 2004-03-25
AU2003215311A1 (en) 2003-09-09
AU2003211129A8 (en) 2003-09-09
KR20040098000A (en) 2004-11-18
AU2003211129A1 (en) 2003-09-09
CN1646449A (en) 2005-07-27
US7067208B2 (en) 2006-06-27
WO2003071619A2 (en) 2003-08-28
WO2003071618A2 (en) 2003-08-28
WO2003071618A3 (en) 2003-12-18
US20030165732A1 (en) 2003-09-04
EP1497871A2 (en) 2005-01-19
US20030180602A1 (en) 2003-09-25
US7144651B2 (en) 2006-12-05
US20030157386A1 (en) 2003-08-21
JP2005518643A (en) 2005-06-23
US7045237B2 (en) 2006-05-16
US20030224238A1 (en) 2003-12-04
US7135248B2 (en) 2006-11-14
AU2003215311A8 (en) 2003-09-09
WO2003071618A9 (en) 2004-02-12
US20050074650A1 (en) 2005-04-07
EP1497871A4 (en) 2008-03-05
US7255956B2 (en) 2007-08-14

Similar Documents

Publication Publication Date Title
US7067208B2 (en) Load matched power generation system including a solid oxide fuel cell and a heat pump and an optional turbine
US20030054215A1 (en) Compact integrated solid oxide fuel cell system
WO2004004055A1 (en) Solid high polymer type cell assembly
JP2004152758A (en) Fuel cell stack having heat exchanger
US7459231B2 (en) Polymer electrolyte fuel cell stack and operating method thereof
JP2008505462A (en) Fuel cell with in-cell humidification
JP6139231B2 (en) Solid oxide electrochemical cell stack structure and hydrogen power storage system
US20210119228A1 (en) Metal Support for Electrochemical Element, Electrochemical Element, Electrochemical Module, Electrochemical Device, Energy System, Solid Oxide Fuel Cell, Solid Oxide Electrolytic Cell, and Method for Manufacturing Metal Support
CN111886730A (en) Metal-supported fuel cell and fuel cell module
JP4797352B2 (en) Solid oxide fuel cell
JP4461955B2 (en) Solid oxide fuel cell
JP2004362800A (en) Fuel cell
WO2009119106A1 (en) Solid oxide fuel cell
WO2012165467A1 (en) Fuel cell module
JP4654631B2 (en) Solid oxide fuel cell
EP4071867A2 (en) Hydrogen pumping proton exchange membrane electrochemical cell with carbon monoxide tolerant anode and method of making thereof
JP6993488B1 (en) Fuel cell power generation system and control method of fuel cell power generation system
JP2005294152A (en) Solid oxide fuel cell
JP2010238440A (en) Fuel battery module
JP2006210151A (en) Fuel cell system
Shim et al. Nafion ionomer-impregnated composite membrane
US20060057434A1 (en) Fuel cell power generation system
JP2006080052A (en) Solid oxide fuel cell
Fukui et al. OCV and methanol crossover in DMFCs
AU2002236214A1 (en) Polymer electrolyte fuel cell stack and operating method thereof

Legal Events

Date Code Title Description
AS Assignment

Owner name: ION AMERICA CORPORATION, CALIFORNIA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:MCELROY, JAMES F.;REEL/FRAME:013794/0791

Effective date: 20030220

AS Assignment

Owner name: BLOOM ENERGY CORPORATION,CALIFORNIA

Free format text: CHANGE OF NAME;ASSIGNOR:ION AMERICA CORPORATION;REEL/FRAME:018345/0543

Effective date: 20060920

Owner name: BLOOM ENERGY CORPORATION, CALIFORNIA

Free format text: CHANGE OF NAME;ASSIGNOR:ION AMERICA CORPORATION;REEL/FRAME:018345/0543

Effective date: 20060920

STCB Information on status: application discontinuation

Free format text: ABANDONED -- AFTER EXAMINER'S ANSWER OR BOARD OF APPEALS DECISION

AS Assignment

Owner name: U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT, CALIFORNIA

Free format text: SECURITY INTEREST;ASSIGNOR:BLOOM ENERGY CORPORATION;REEL/FRAME:037301/0093

Effective date: 20151215

Owner name: U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGEN

Free format text: SECURITY INTEREST;ASSIGNOR:BLOOM ENERGY CORPORATION;REEL/FRAME:037301/0093

Effective date: 20151215

AS Assignment

Owner name: BLOOM ENERGY CORPORATION, CALIFORNIA

Free format text: RELEASE BY SECURED PARTY;ASSIGNOR:U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT;REEL/FRAME:047686/0121

Effective date: 20181126