DE69019528D1 - Verbrennungsvorrichtung und arbeitsweise für eine integrierte energieeinheit. - Google Patents

Verbrennungsvorrichtung und arbeitsweise für eine integrierte energieeinheit.

Info

Publication number
DE69019528D1
DE69019528D1 DE69019528T DE69019528T DE69019528D1 DE 69019528 D1 DE69019528 D1 DE 69019528D1 DE 69019528 T DE69019528 T DE 69019528T DE 69019528 T DE69019528 T DE 69019528T DE 69019528 D1 DE69019528 D1 DE 69019528D1
Authority
DE
Germany
Prior art keywords
combustion device
energy unit
integrated energy
integrated
unit
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.)
Expired - Fee Related
Application number
DE69019528T
Other languages
English (en)
Other versions
DE69019528T2 (de
Inventor
Reinhard Klaass
Bert Minshall
Francis Suriano
William Caan
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.)
Honeywell International Inc
Original Assignee
AlliedSignal Inc
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 AlliedSignal Inc filed Critical AlliedSignal Inc
Publication of DE69019528D1 publication Critical patent/DE69019528D1/de
Application granted granted Critical
Publication of DE69019528T2 publication Critical patent/DE69019528T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/14—Gas-turbine plants having means for storing energy, e.g. for meeting peak loads
    • F02C6/16—Gas-turbine plants having means for storing energy, e.g. for meeting peak loads for storing compressed air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27—Fluid drives
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/16—Mechanical energy storage, e.g. flywheels or pressurised fluids
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
DE69019528T 1989-09-21 1990-09-20 Verbrennungsvorrichtung und arbeitsweise für eine integrierte energieeinheit. Expired - Fee Related DE69019528T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/411,334 US5274992A (en) 1989-09-21 1989-09-21 Integrated power unit combustion apparatus and method
PCT/US1990/005356 WO1991004446A1 (en) 1989-09-21 1990-09-20 Integrated power unit combustion apparatus and method

Publications (2)

Publication Number Publication Date
DE69019528D1 true DE69019528D1 (de) 1995-06-22
DE69019528T2 DE69019528T2 (de) 1996-01-25

Family

ID=23628508

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69019528T Expired - Fee Related DE69019528T2 (de) 1989-09-21 1990-09-20 Verbrennungsvorrichtung und arbeitsweise für eine integrierte energieeinheit.

Country Status (6)

Country Link
US (1) US5274992A (de)
EP (1) EP0491877B1 (de)
JP (1) JP2519620B2 (de)
CA (1) CA2065158C (de)
DE (1) DE69019528T2 (de)
WO (1) WO1991004446A1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5274996A (en) * 1991-10-11 1994-01-04 Allied-Signal, Inc. Closed loop fuel control system
US6305156B1 (en) * 1999-09-03 2001-10-23 Alliedsignal Inc. Integrated bleed air and engine starting system
US6960848B2 (en) * 2003-05-09 2005-11-01 Nisca Corporation Electromagnetic drive device and light quantity adjustment device using the same
US6968697B2 (en) * 2003-09-17 2005-11-29 Honeywell International Inc. Integral compressor housing of gas turbine engines
US7442006B2 (en) * 2005-08-15 2008-10-28 Honeywell International Inc. Integral diffuser and deswirler with continuous flow path deflected at assembly
US20070169461A1 (en) * 2006-01-19 2007-07-26 Honeywell International Inc. Catalytic bipropellant hot gas generation system
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
FR2990414B1 (fr) * 2012-05-10 2015-04-10 Microturbo Procede de fourniture de puissance auxiliaire par un groupe auxiliaire de puissance et architecture correspondante
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
US10323577B2 (en) * 2015-02-23 2019-06-18 Rolls-Royce North American Technologies, Inc. Self-cooled gas bottle
US9920695B2 (en) * 2015-06-22 2018-03-20 Exhaustless Inc. Thrust recovery in airplanes
US10836505B2 (en) * 2016-06-23 2020-11-17 Raytheon Technologies Corporation Operating auxiliary power unit during off-nominal propulsion system operation
US11028773B2 (en) 2018-02-22 2021-06-08 Rolls-Royce North American Technologies Inc. Compressed gas integrated power and thermal management system

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2655788A (en) * 1946-10-07 1953-10-20 Rateau Soc Turbine gas engine adapted to operate with or without atmospheric air chiefly for the propulsion of warships
GB798704A (en) * 1954-12-23 1958-07-23 Snecma Improvements in or relating to a unit for starting aircraft gas turbine engines
GB1072485A (en) * 1963-05-03 1967-06-14 Plessey Uk Ltd Improvements in or relating to engine-starter and auxiliary drive systems
FR1388004A (fr) * 1963-11-27 1965-02-05 Dispositif de démarrage et de contrôle du fonctionnement d'un générateur de puissance à turbine à gaz
GB1136584A (en) * 1966-01-19 1968-12-11 Rolls Royce Gas turbine engine accessory drive systems
US3439495A (en) * 1967-09-18 1969-04-22 Robert L Binsley Resonating combustor for directly starting turbine engine
GB1309077A (en) * 1969-05-19 1973-03-07 Plessey Co Ltd Combined auxiliary power and engine starter systems
US3662975A (en) * 1970-09-21 1972-05-16 Robert E Driskill Auxiliary electrical generating system for jet aircraft
US3965673A (en) * 1973-05-19 1976-06-29 Vereinigte Flugtechnische Werke-Fokker Gesellschaft Mit Beschrankter Haftung Apparatus for starting aircraft engines and for operating auxiliary on-board power generating equipment
AT358335B (de) * 1975-10-03 1980-09-10 Gilli Paul Viktor Dipl Ing Dr Einrichtung zum schnellanfahren und/oder zum kurzzeitigen ueberlasten eines gasturbinen- satzes mit offener prozessfuehrung
US4441028A (en) * 1977-06-16 1984-04-03 Lundberg Robert M Apparatus and method for multiplying the output of a generating unit
US4312179A (en) * 1978-05-05 1982-01-26 Bbc Brown, Boveri & Company, Ltd. Gas turbine power plant with air reservoir and method of operation
US4237692A (en) * 1979-02-28 1980-12-09 The United States Of America As Represented By The United States Department Of Energy Air ejector augmented compressed air energy storage system
US4628687A (en) * 1984-05-15 1986-12-16 A/S Kongsberg Vapenfabrikk Gas turbine combustor with pneumatically controlled flow distribution
DE3424141A1 (de) * 1984-06-30 1986-01-09 BBC Aktiengesellschaft Brown, Boveri & Cie., Baden, Aargau Luftspeicher-gasturbine
JPH0663646B2 (ja) * 1985-10-11 1994-08-22 株式会社日立製作所 ガスタ−ビン用燃焼器
US4777793A (en) * 1986-04-14 1988-10-18 Allied-Signal Inc. Emergency power unit
US4815277A (en) * 1987-01-08 1989-03-28 Sundstrand Corporation Integrated power unit
US4759178A (en) * 1987-03-17 1988-07-26 Williams International Corporation Aircraft auxiliary power unit
JPS6469721A (en) * 1987-09-02 1989-03-15 Sundstrand Corp Multipurpose auxiliary power device
US5309708A (en) * 1988-06-03 1994-05-10 Alliedsignal Inc. Multifunction integrated power unit

Also Published As

Publication number Publication date
EP0491877B1 (de) 1995-05-17
DE69019528T2 (de) 1996-01-25
JPH05502081A (ja) 1993-04-15
EP0491877A1 (de) 1992-07-01
WO1991004446A1 (en) 1991-04-04
CA2065158C (en) 1996-04-09
US5274992A (en) 1994-01-04
JP2519620B2 (ja) 1996-07-31

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee