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Publication numberUS3251403 A
Publication typeGrant
Publication dateMay 17, 1966
Filing dateJan 5, 1962
Priority dateJan 5, 1962
Publication numberUS 3251403 A, US 3251403A, US-A-3251403, US3251403 A, US3251403A
InventorsGail P Smith
Original AssigneeCorning Glass Works
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Ceramic heat exchanger structures
US 3251403 A
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Description  (OCR text may contain errors)

May 17, 1966 G. P. SMITH CERAMIC HEAT EXCHANGER STRUCTURES Filed Jan.

INVENTOR.

GA/L P. SM/TH Ace/ um. A77 0RNEK5 GM 1? 7 8mm,

United States Patent CERAMIC HEAT EXCHANGER STRUCTURES Gail P. Smith, Corning, N .Y., assignor to Corning Glass Works, Corning, N.Y., a corporation of New York Filed Jan. 5, 1962, Ser. No. 164,572 4 Claims. (Cl. 165-10) This invention relates to heat exchangers and in particular it concerns regenerative heat exchanger bodies particularly useful for application with gas turbines.

It is the primary object of the present invention to provide heat exchanger bodies composed of thin walled ceramic material, that are lightweight, are inexpensive, are characterized by a low coeflicient of thermal expansion, and are chemically and thermally durable.

These and other objects are attained in accordance with this invention in which a thin walled ceramic honeycomb is formed from ceramic materials hereinafter described in detail, and is provided with a protective covering cemented to several of its surfaces. The honeycomb body is characterized by a plurality of unobstructed gas flow paths extending through it to a pair of opposed, substantially parallel surfaces. The term unobstructed as used in this application means that the flow paths have no internal structure that, for example, would stop gas flow. The unobstructed flow paths can be characterized as desired and may be linear, tortuous or the like. These gas paths are separated from one another by thin walls of the ceramic material. The specific design of the structure coupled with the character of the ceramic materials in the completed product result in a body uniquely suited as a regenerative heat exchanger for application at high and rapidly changing temperatures such as are encountered in gas turbine operation.

The invention will be most readily understood upon considering its detailed description in conjunction with.

the attached drawing in which: a

FIG. 1 is a schematic representation of a heat exchanger and auxiliary equipment showing the flow of gas therethrough;

FIG. 2 is a perspective view of a heat exchange body of the invention in which the channels are arranged for axial flow;

FIG. 3 is a perspective view of a second embodiment of the heat exchange body in which the channels are arranged for radial flow; and

FIG. 4 is a perspective view of a honeycomb segment that can be used in making a radial flow heat exchanger.

Referring now to FIG. 1, fresh intake gas is fed by a line to a compressor 11 wherein its temperature and pressure are raised. The gas from compressor 11 then is passed through line 11a into a first portion 12 of a.

heat exchanger body 13 heated to a high temperature as hereinafter described. In that portion of the heat exchanger 13, the gas is heated by the heat in the ceramic walls defining the gas flow paths and emerges at the opposite surface through line 14 at a higher temperature. The highly heated gas is then passed to :a burner 15 where its temperature is further raised by combustion. The hot gas from the burner is then expanded through a turbine 16 where part of its energy is converted to work. The exhaust gas from the turbine is conducted through line 17 into a relatively cool portion 18 of the heat exchanger body 13 where it gives up a substantial portion of its heat. Gas from this portion of the heat exchanger body is exhausted through a line 19. It is to be noted that the heat exchanger body 13 is rotated in use; accordingly, after one portion of it has been heated from the gases exhausted by the turbine, that heated portion rotates to the compressor inlet where the gas fed from the compressor can recover the heat. The two portions 12 and 18 are divided from one another by the stationary seal 20 extending across the top and bottom surfaces by thin walls of ceramic material 26. At its hub or axial bore and along its outside surface, the honeycomb body is covered with, respectively, a hub wall 30 and a rim wall 32. The hub and rim walls or members 30 and 32 are cemented to the honeycomb body by a cement 34 that is foamed in place. The heat exchanger body of FIG. 2 can be .rotated by means, not shown, bearing on the hub, on the rim or on both. I

For a radial flow heat exchanger, the gas channels I extend radially of the central axis of the cylindrical or annular shaped honeycomb body such as is shown in FIG. 3. The honeycomb is characterized by a plurality of unobstructed gas flow paths 36 separated from one another by thin ceramic walls 37 and extending from the central wall 38 outwardly and terminating in the outer surface 39. Where the honeycomb of a radial flow heat exchanger body is essentially one piece, the top and bottom surfaces are covered with rim members 44 that are cemented to the honeycomb structure by a foamed ceramic cement 46. Rotation of the radial flow heat exchanger body is achieved by use of members, not shown, that may apply rotational force on the rims.

For some purposes it is desirable to have the radial flow heat exchanger body made of a plurality of segments. For example, if a part of the body should be damaged, a segmented honeycomb body can be readily repaired by simple replacement of the damaged segment. A segment of the type from which such a honeycomb body can be assembled is shown in FIG. 4. In the embodiment of FIG. 4, the segment comprises a truncated pyramidal body having channels 50 extending between two of its parallel surfaces 51 and 52. The other external surfaces are covered with a rim member 53 that,

as before, is cemented to the honeycomb body by a V achieved by using covering members, such as those shown at 44 in FIG. 3, cemented to the assembled segments.

Ceramic honeycomb bodies that are useful in accordance with the teachings of this invention can be prepared by several processes. For example, a pulverized ceramic material can be admixed with a suitable binder and then extruded to a ribbon form. The resulting ribbon can be further shaped if desired, and assembled, cit-her by itself or with other ribbons of this material to the desired honeycomb shape. The resulting assembly is then sintered to a unitary structure. Preferably, however, the ceramic honeycomb body is prepared by coating a suitable carrier with a mixture of a pulverized ceramic and a binder, crimping the resulting coated carrier and then assembling it to the desired shape alone or with another coated carrier that need not be crimped. The assembled body is then heated to a temperature sufficient to sinter it to a unitary structure as more fully detailed hereinafter. This latter procedure is, generally, the process set forth in the copending application of Robert Z. Hollenbach, Serial 3 Number 759,706, filed September 8, 1958, and now Patent Number 3,112,184 granted November 26, 1963.

The purpose of the binder is to bond the unfired ceramic material to the carrier, to impart green strength to the coated carrier and to retain the formed unfired article in the desired shape after forming and prior to sintering. In order that the resultant article be essentially all ceramic material having'a low coeflicient of thermal expansion, it is preferred to use an organic binder, especially those that are heat curable or thermosetting, that can be removed by decomposition and/ or volatilization when the article is fired. Among the many materials having the requisite, well known characteristics of binders, that can be used in the process are such natural materials as gum arabic, colophony and shellac and such synthetic organic resins as acrylate resins, methacrylate resins, alkyd resins, cellulose derivatives, coumarone indene resin, phenolic resins, polyamides, polyesters, resorcinol resins, styrene resins, terpene resins, urea resins, vinyl resins, chlorinated paraffins and melamine resins.

The purpose of the carrier is to provide support for the unfired coating to allow it to be formed to the desired shape prior to sintering the ceramic coating. Tea bag paper is a preferred carrier and a list of other suitable materials is disclosed in the aforementioned Hollenbach patent application, to which reference can be made. Tea bag paper, as well as other organic film materials, substantially decompose upon firing and thus result in an article consisting almost entirely of ceramic material.

In order to produce a structure in accordance with the present invention having characteristics suitable for a heat exchanger body, it is essential that ceramic materials be used that have a low coefiicient of thermal expansion in the fired state on the order of about minus to plus 10 times 10"'/ C. over an extended temperature range. Suitable ceramic materials for this purpose include lithium aluminosilicates such as, for example, glass or crystalline petalite and beta spodumene, glass-ceramics having a lithium aluminosilicate base and especially those made in accordance with Example 1 of United States patent to Stookey, Number 2,920,971, as well as mixtures of any of the foregoing materials. Petalite glass-ceramic mixtures generally include about 10 to 40 weight percent of the glass-ceramic and the remainder petalite. Beta spodumene-petalite mixtures usually contain about 1 to 4 parts of petalite for each 4 to 1 parts of beta spodumene. These materials normally are used in a particle size of about minus 200 mesh (Tyler) or finer, depending on the wall thickness desired in the resulting article.

Structures are assembled from ceramic coated carriers in a variety of ways, and the resulting structures are called honeycombs, a term which in this specification means a unitary body having a multitude of unobstructed gas paths of any predetermined size and shape, each such gas path being defined by ceramic walls and extending to opposed essentially parallel surfaces. These structures can be assembled from multiple layers of film corrugated with the same pattern with alternate layers laterally disposed a distance equal to half of the width of the individual pattern so that layers do not nest with each other. The honeycomb structure can also be formed from rolling alternate layers of crimped and uncrimped coated carriers until the desired shape is formed. A structure can also be formed by assembling to a stack alternate crimped and uncrimped coated carriers until the desired dimensions are attained. Other .ways of assembling these honeycombs will be apparent to those skilled in the art.

The firing of the green structure or matrix, however formed, is accomplished in the normal manner for ceramic firing by placing the article in a furnace and heating it at a rate slow enough to prevent breakage due to thermal shock to a temperature high enough to cause the ceramic particles to sinter. While the firing schedule, including heating rates and sintering temperatures, will vary depending upon the ceramic material utilized, the size and shape of the article formed, and the atmosphere used, the details of such schedules are not critical and suitable conditions are readily determinable by one skilled in the art of firing ceramic articles.

, As noted hereinbefore, the surfaces of the honeycomb body other than those where the gas flow paths terminate are covered. These covering members, sometimes termed rims or hubs, can be formed in any desired manner. A preferred method of preparation involves forming a slip, suitably of the same composition as the ceramic used in the honeycomb body or of a glass such as the borosilicate glasses disclosed in the United States patent to Hood et a1. Number 2,106,744, and slip casting to the desired shape. Another suitable procedure involvesheat sagging strips composed, for example, of the aforementioned borosilicate glass, to arcuate sections. Then several, e.g. four or more, arcuate sections are assembled to the desired shape and the abutting ends are joined by heat sealing.

The rim and hub or other cover members are attached to the honeycomb body by use of a ceramic cement that will foam and readily bond those members and that has a low coefficient of thermal expansion in the foamed state. Cement for this purpose has a composition, by weight, of 1 to 16 percent of lead oxide, 1 to 15 percent of a flux, 1 to 6 percent of silicon carbide, 1 to 6 percent of S0 and substantially all of the remainder, and at least about percent of the total cement composition, a lithium-aluminosilicate ceramic such as glassy or cystalline petalite, a glassy ceramic having such a base composition or any combination of the foregoing. Glass petalite is the preferred ceramic. Typical flux ma terials include the fluorides and oxides of magnesium, calcium, strontium, barium, zinc, cadmium, lead, lithium, sodium and pottassium. Suitably a mixture of oxide and fluoride fluxes is used. The S0 content of the batch is provided by, for example, a compound such as calcium sulfate, barium sulfate, strontium sulfate or lithium sulfate. It will be apparent that the use of any of these compounds provides both the S0 and an oxide flux. Lead sulfate, which also may be used, provides the essential lead oxide and S0 The cement is used by pouring it into the spaces between the parts to be joined and then firing the unit to a temperature of about 1050 to 1150 C. until foaming and sintering are complete. Thereafter, the unit is cooled to handling temperature.

The invention will be described further in conjunction with the following example in which the details are given by way of illustration and not by way of limitation.

In this example, a ceramic composition is made of parts by Weight of petalite and 25 parts by weight of a glass-ceramic having the following approximate composition by oxide analysis in weight percent: 70 percent SiO 18 percent A1 0 5 percent TiO 3 percent Li O, 3 percent MgO and 1 percent ZnO. The composition is ball-milled to a minus 200 mesh (Tyler) particle size. A solution of the following composition is added to 2160 grams of the ceramic material in the ball mill:

640 cc. 860 cc.

Versamid is the trade name of a thermoplastic polymer supplied by General Mills, Inc. It is prepared by condensation of polymerized unsaturated fatty acids, such as dilinoleic acid, with aliphatic amines such as ethylene diamine.

The ceramic material and the binder are further ballmilled for about three hours to produce a uniform suspension. A porous natural cellulose paper, commonly known as 3 /2 pound tea bag paper, out to a width of 4 inches is then dipped into the suspension and dried by heating to C. for 2 minutes. The dried, coated paper is then heated to C. and crimped to produce a pattern, taken in cross-section, in the shape of an isosceles triangle with legs about 0.07 inch long and an open base about 0.1 inch wide. The crimped, unfired, coated paper is rolled up simultaneously with a sheet of tea bag paper of the same width, which has been coated in the same manner but not crimped, upon a 2-inch diameter reel until an annular cylinder with an outside diameter of about 23 inches is obtained. Preferably, the uncrimped coated paper is not dried prior to the roll-up operation, but this paper is dried by forcing air heated to about 120 C. through the channels of the annular cylinder as they are formed during the roll up operation.

The unfired matrix body is then placed in a sealed furnace chamber and heated in accordance with the following schedule:

Temperature range: Firing rate Room temp. to 700 C. 350 C./hr. Hold at 700 C n 1 hour. 700 C. to 1220 C. Furnace rate. Hold at 1220 C 30 minutes. Cool to room temp. Furnace rate. Refire to 1240 C. 300 C./hr. Hold at 1240 C. 7 hours.

The sintered article is then cooled to handling temperature and removed from the furnace.

Rim and hub members are made for the foregoing honeycomb from a slip of the glass-ceramic used in preparing the honeycomb. The slip is cast in annular molds of a size to fit the honeycomb with about one-eighth inch clearance. After drying, the molds are removed and the cast structures are fired at about 1250 C.

The rim, hub and honeycomb are assembled. Then a cement having the following composition by weight is used to join these members: 9.23 percent of zinc fluoride, 1.28 percent of calcium fluoride, 3.42 percent of silicon carbide, and the remainder petalite that had been fused with lead sulfate in an amount such that it contained 8 percent of lead oxide and 2.87 percent of S A batch of this cement composition is dispersed in a mixture containing 75 weight percent of butyl alcohol and 25 weight percent of toluene and is wet ball-milled to thoroughly mix the batch. This cement is poured in the annular spaces in the assembly. The resulting assembly is then placed in a furnace and raised to 100 C. at a rate of 2 C./min. After 2 hours at 100 C., the temperature is raised at 5 C/minute to 1t100 C. and is held at 1100 C. for one hour and 15 minutes to permit the foaming action to be completed. It is then furnace cooled at a rate of 5 C./min. to handling temperature.

Honeycomb bodies formed to heat exchanger members as just detailed are characterized by an extremely large number of gas channels per unit of surface area. Quite commonly, a square foot of the surface of the honeycomb will have over 57,000 channels. As is evident, therefore, most of the cross section is void and the resulting units are relatively lightweight, having a density on the order of about 30 pounds per cubic foot. These bodies made with the ceramic materials hereinbefore specified have a low coefiicient of thermal expansion of about minus to about plus 10 10* C. over a range up to about 300 C., and may actually be zero. It is accordingly, evident that these bodies can be subjected to tremendous thermal shock as by repeated thermal cycling to over 1000 C., a temperature beyond usual gas turbine operating temperatures, without adverse efiect. The excellent chemical durability of the structure allows its extended use despite the corrosive conditions experienced in the application contemplated.

ized by a low coefficient of thermal expansion and therefore can readily be produced to fixed dimensions and used, as by rotating it, without concern about developing a poor fit. The invention is further advantageous in that these unique results are achieved with readily available and inexpensive raw materials while applying skills available to artisans in the ceramic arts. Unless otherwise stated or apparent, all percentages and parts given in the foregoing description are by weight.

In accordance with the provisions of the patent statutes, I have explained the principles of my invention and have illustrated and described what I now considered to be its best embodiment. However, I desire to have it understood that, within the scope of the appended claims, the invention may be practiced otherwise than as specifically illustrated and described.

I claim:

1. A rotatable, annular-shaped heat exchanger body comprising a thin walled ceramic honeycomb having two pairs of substantially parallel opposing surfaces and a plurality of unobstructed gas passages extending between and terminating in a first pair of said opposing substantially parallel surfaces, said gas passages being defined by thin walls of said ceramic, rigid covering members on each of the other pair of opposing surfaces, and a foamed ceramic cement joining said covering members to said honeycomb, said covering members, ceramic honeycomb and'foamed ceramic cement all having a low and essentially similar coeflicient of thermal expansion.

=2. A heat exchanger body in accordance with claim 1 in which said unobstructed gas passages are essentially parallel to the central axis of saidheat exchanger body.

3. A heat exchanger body in accordance with claim 1 in which said unobstructed gas passages are essentially radial to the central axis of said heat exchanger body.

4. A rotatable, annular-shaped heat exchanger body formed of a plurality of ceramic honeycomb segments each having a rectangular base pyramidal shape truncated parallel to its base and a plurality of unobstructed gas passages extending between the base and its parallel surface, said segments being assembled to an annular shaped body with the collected bases thereof constituting the external wall, a ceramic covering member on each of the surfaces of each segment other than its base and the surface parallel thereto, a foamed ceramic cement joining said ceramic covering members to said honeycom'b segments, and means retaining said assembled segments in position relative to one another, said ceramic honeycomb segments, said covering members and said foamed ceramic cement all having a low and essentially similar coefiicient of thermal expansion.

References Cited by the Examiner UNITED STATES PATENTS 3,081,822 3/1963 Wolansky et al. 10

FOREIGN PATENTS 750,303 6/ 1956 Great Britain. 811,434 4/1959 Great Britain.

FREDERICK L. MATTESON, JR., Primary Examiner. CHARLES SUKALO, Examiner.

Patent Citations
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US3081822 *Apr 14, 1960Mar 19, 1963Thompson Ramo Wooldridge IncRotary regenerator drum fabrication
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Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3367404 *Dec 8, 1966Feb 6, 1968Gen Motors CorpRadial flow regenerator matrix formed from ceramic blocks and the method of making
US3382915 *May 17, 1965May 14, 1968Gen Motors CorpRotary regenerator
US3634111 *Sep 16, 1969Jan 11, 1972Corning Glass WorksGlass-ceramic cements comprising silicon carbide
US3715220 *Mar 19, 1969Feb 6, 1973Corning Glass WorksCeramic article and method of making it
US3819439 *Oct 5, 1972Jun 25, 1974Hexcel CorpMethod of making honeycomb of sinterable material employing stepwise coating of a resin-containing composition
US3899555 *Dec 27, 1971Aug 12, 1975Nissan MotorMethod of preparing ceramic structures
US3923940 *Mar 28, 1973Dec 2, 1975Nippon Toki KkProcess for the manufacture of ceramic honeycomb structures
US3926702 *Mar 27, 1973Dec 16, 1975Asamura Patent OfficeCeramic structures and process for producing the same
US3929494 *Dec 22, 1972Dec 30, 1975Owens Illinois IncSealant for glass-ceramic surfaces
US3939902 *Feb 5, 1975Feb 24, 1976Coors Porcelain CompanyHeat exchanger rim and hub with L-shaped cross-section
US3951670 *Feb 10, 1975Apr 20, 1976Corning Glass WorksCristobalite suppression in high-silica Li2 O-Al2 O-SiO2 devitrified glass frits
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US4233351 *May 15, 1979Nov 11, 1980Nippon Soken, Inc.Ceramic honeycomb structure
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US4357987 *Jul 27, 1981Nov 9, 1982Ngk Insulators, Ltd.Thermal stress-resistant, rotary regenerator type ceramic heat exchanger and method for producing same
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US5575067 *Feb 2, 1995Nov 19, 1996Hexcel CorporationMethod of making a continuous ceramic fiber reinforced heat exchanger tube
US5881775 *Jan 2, 1997Mar 16, 1999Hexcel CorporationHeat exchanger tube and method for making
US6347453May 24, 1999Feb 19, 2002Matthew P. MitchellAssembly method for concentric foil regenerators
US8092579Oct 9, 2008Jan 10, 2012Dow Global Technologies LlcThermal shock resistant soot filter
US20120067556 *Sep 22, 2010Mar 22, 2012Raytheon CompanyAdvanced heat exchanger
DE3104945A1 *Feb 11, 1981Apr 8, 1982Isartaler SchraubenkompressorAir cooler having a condensate trap
Classifications
U.S. Classification165/10, 264/630, 428/116, 165/DIG.430, 165/180, 156/89.22, 501/80
International ClassificationF28D19/04, F28F21/04
Cooperative ClassificationY10S165/043, F28F21/04, F28D19/04
European ClassificationF28D19/04, F28F21/04