US3511309A - Rotary regenerator - Google Patents

Rotary regenerator Download PDF

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US3511309A
US3511309A US777264A US3511309DA US3511309A US 3511309 A US3511309 A US 3511309A US 777264 A US777264 A US 777264A US 3511309D A US3511309D A US 3511309DA US 3511309 A US3511309 A US 3511309A
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Prior art keywords
matrix
face
seal
regenerator
seals
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Expired - Lifetime
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US777264A
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Hugh J Clifford
George H Johnson
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Motors Liquidation Co
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Motors Liquidation Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D19/00Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
    • F28D19/041Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier with axial flow through the intermediate heat-transfer medium
    • F28D19/042Rotors; Assemblies of heat absorbing masses
    • 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
    • Y10S165/00Heat exchange
    • Y10S165/009Heat exchange having a solid heat storage mass for absorbing heat from one fluid and releasing it to another, i.e. regenerator
    • Y10S165/013Movable heat storage mass with enclosure
    • Y10S165/016Rotary storage mass
    • Y10S165/02Seal and seal-engaging surface are relatively movable
    • Y10S165/021Seal engaging a face of cylindrical heat storage mass

Definitions

  • regenerators particularly those of the axial-flow type.
  • Such regenerators include a matrix which is a disk or drum of material pervious to flow through it in an axial direction, the matrix being rotated about its axis so as to cause each element of the matrix to pass alternatively through passages conveying fluids at different temperatures. Heat is stored in the matrix while exposed to one fluid and is delivered to the other fluid when it passes through it.
  • seals at the rims of the matrix to prevent flow around the matrix rather than through it.
  • Such seals may extend entirely around the matrix on each side or may extend only part way around the matrix on one of the two sides. It is important that these seals bear lightly against the matrix to minimize friction and wear but that they be in contact to minimize leakage.
  • this difiiculty is cured by providing a structure in the matrix which renders those portions of the matrix which contact the by-pass seal at the outer margin of the matrix impervious to fluid flow or transmission of pressure from one face to the other.
  • the matrix is of a ceramic type and the blockage is eifected by cutting a channel into the outer circumferential portion of the matrix between the faces, which channel is filled with a ceramic material which is fired and hardened to form a barrier impenetrable to fluid between the faces of the matrix.
  • Our invention provides for such blockage in a regenerator matrix of metal construction embodying metal sheets some of which have corrugations extending axially of the matrix.
  • the principal objects of our invention are to improve the performance of rotary regenerators, to provide more precise and effective control over the contact forces of seals for such regenerators, to improve durability and minimize leakage in regenerators, and to provide a simple and effective means for eliminating imposition of static pressure from one face of a matrix on a seal which bears against the opposite face. While the principles of the invention may be applied to radial-flow regenerators, it is more readily applied to and more likely to find useful application in axial-flow regenerators, and is so shown.
  • FIG. 1 is a sectional view of a rotary regenerator taken in a plane containing the axis of rotation thereof.
  • FIG. 2 is a fragmentary elevation view of one face of a matrix, with parts cut away.
  • FIG. 3 is a fragmentary enlargement of FIG. 1.
  • FIG. 4 is a fragmentary axonometric view of a matrix.
  • a gas turbine engine may include an engine block or housing 9 which supports the rotating parts and combustion chamber of the engine (not illustrated) and which also supports a rotary regenerator R including an axial-flow matrix 10.
  • the matrix is mounted for rotation about a horizontal axis, as illustrated, at a side face of the block 9.
  • the matrix is enclosed by the block 9 and a regenerator cover 11 fixed to the block, these two constituting a housing for the matrix.
  • the regenerator cover defines a cool air inlet 13 and an exhaust outlet 14.
  • the block 9 defines a hot air outlet 15 opposite to the inlet 13 and a hot gas inlet 17 opposite to the exhaust outlet 14.
  • the matrix 10 is of known type embodying a hub or inner ring 18 by which it is driven, an annulus 19 of heat exchange material defining passages extending generally parallel to the axis from face to face of the matrix, and an outer ring or outer rim 20.
  • the heat exchange material 19 is fixed to the hub 18.
  • Seals cooperating with the matrix include an outer side rim seal 23 engaging the matrix adjacent the rim, an outer side hub seal 24 engaging the hub, an inner side rim seal 25 opposite to (Pat. No. 3,476,173) are seal 23, and an inner side hub seal 26 opposite to seal 24.
  • the sealing structure also includes radial crossarm seals extending from the hub to the outer margin of the matrix (not illustrated) to block flow from one fluid passage to the other across the face of the matrix. These seals may be as described in Pat. No. 3,368,611.
  • the means for driving and supporting the matrix illustrated is the same as one form shown in the prior application referred to above. It includes a shaft 30 rotatably mounted in the housing driven by a sprocket 31. An inner coupling member 34 fixed on the shaft is coupled by a flexible connection to an outer coupling member 35 which connects the shaft to the hub 18 of the matrix.
  • the sheet metal matrix is of such a nature as to provide numerous small passages or pores 37 extending parallel to the axis of the matrix.
  • this structure is made by laying up alternate spirals 39 of flat sheet metal and 40 of corrugated sheet metal, which are then bonded together by brazing.
  • the means for blocking transmission of pressure from face to face of the matrix through the marginal part engaged by the rim seals is shown particularly in FIGS. 3 and 4.
  • the radially outer portion 50 of the matrix between seals such as 23 and 25 embodies alternating flat sheets 51 and corrugated sheets 53.
  • the corrugated sheets may be similar to those in the main portion 19 3 of the matrix but, in general, the corrugations in the blocked outer portion are shallow while those in the inner portion may not be.
  • the corrugated sheets 53 are provided with two ridges or corrugations 57 and 58 extending lengthwise of the corrugated strip and circumferentially of the matrix, crossing the normal corrugations of the strip which extend axially of the matrix.
  • the circumferential 1y extending ridges 57 and 58 as can clearly be seen, out off or block the passages which otherwise would exist between adjacent flat sheets 51.
  • the peaks of outward extending ridge 58 bear tightly against and are brazed to the next adjacent fiat sheet 51 outward of the corrugated sheet and the peaks of corrugations of ridge 57 similarly bear against the next inner flat sheet 51.
  • the two ridges block the otherwise existing flow passages on both the outer and inner sides of the corrugated sheet 53.
  • the ridges 57 and 58 may be provided during the rolling to provide the normal corrugations of the sheet or may be added by a subsequent rolling operation.
  • a rotary regenerator comprising, in combination, a housing, an axial-flow matrix having radial faces and an outer circumferential surface, the matrix including heat-exchange material defining multifarious distinct generally parallel passages from face to face of the matrix, means mounting the matrix rotatably in the housing, and seal means mounted on the housing engaging at least one face of the matrix adjacent the outer surface of the matrix; the matrix including a peripheral annular zone cooperating with the said seal means, the said peripheral zone comprising alternating smooth and corrugated metal strips with the corrugated strips spacing the metal strips and defining passages across the matrix, the corrugated strips in the said zone having oppositely directed circumferential ridges blocking the said passages so as to isolate the matrix-engaging surface of the seal means from exposure to pressure communicated through the matrix from the remote face of the matrix.
  • regenerator as recited in claim 1 in which the ridges are spaced inwardly from the faces of the matrix.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Description

May 12., 1970 H. J. CLIFFORD ET AL 3,511,309
ROTARY REGENERATOR Filed Nov. 20, 1968 INVENTORS United States Patent 3,511,309 ROTARY REGENERATOR Hugh J. Clifford, Lockport, and George H. Johnson,
Newfane, N.Y., assignors to General Motors Corporation, Detroit, Mich., a corporation of Delaware lh'led Nov. 20, 1968, Ser. No. 777,264
Int. Cl. F28d 19/00 US. Cl. 165-9 2 Clalms ABSTRACT OF THE DISCLOSURE An annular matrix in an axial-flow regenerator which cooperates with circumferential seals bearing against the faces of the matrix at the outer rim has an impervious ring in the matrix structure blocking communication of pressure from one face of the matrix to the matrix-engaging face of the seal at the other face. The blockage is produced by a circumferential corrugation or crimp in the sheets of the matrix which have corrugations extending axially of the matrix.
Our invention relates to rotary regenerators, particularly those of the axial-flow type. Such regenerators include a matrix which is a disk or drum of material pervious to flow through it in an axial direction, the matrix being rotated about its axis so as to cause each element of the matrix to pass alternatively through passages conveying fluids at different temperatures. Heat is stored in the matrix while exposed to one fluid and is delivered to the other fluid when it passes through it. It is customary to provide seals at the rims of the matrix to prevent flow around the matrix rather than through it. Such seals may extend entirely around the matrix on each side or may extend only part way around the matrix on one of the two sides. It is important that these seals bear lightly against the matrix to minimize friction and wear but that they be in contact to minimize leakage.
Communication of pressure between the two faces of the matrix upsets the action of the seals. If the pressures can be communicated from face to face through the matrix to the seals, the effect is to provide communication through a connecting passage such that the pressure distribution exerted on the matrix-engaging face of the inner seal is no longer independent of the pressure distribution exerted against the matrix-engaging face of the outer seal.
According to an invention of Bracken and Hubble disclosed in US. patent application Ser. No. 671,267 for Rotary Regenerator, filed Sept. 28, 1967 (Pat. No. 3,482,- 622) this difiiculty is cured by providing a structure in the matrix which renders those portions of the matrix which contact the by-pass seal at the outer margin of the matrix impervious to fluid flow or transmission of pressure from one face to the other. In their preferred structure, the matrix is of a ceramic type and the blockage is eifected by cutting a channel into the outer circumferential portion of the matrix between the faces, which channel is filled with a ceramic material which is fired and hardened to form a barrier impenetrable to fluid between the faces of the matrix.
Our invention provides for such blockage in a regenerator matrix of metal construction embodying metal sheets some of which have corrugations extending axially of the matrix.
Our invention is illustrated here as embodied in a rotary regenerator of the type to which US. Pat. No. 3,368,611 of Bracken and Zeek for Regenerator Seals, Feb. 13, 1968, and Bracken and Hubble application Ser. No. 661,075, filed Aug. 16, 1967, for Rotary Regenera- 3,511,309 Patented May 12, 1970 tor Matrix Mount and Drive directed.
The principal objects of our invention are to improve the performance of rotary regenerators, to provide more precise and effective control over the contact forces of seals for such regenerators, to improve durability and minimize leakage in regenerators, and to provide a simple and effective means for eliminating imposition of static pressure from one face of a matrix on a seal which bears against the opposite face. While the principles of the invention may be applied to radial-flow regenerators, it is more readily applied to and more likely to find useful application in axial-flow regenerators, and is so shown.
The nature of our invention and its advantages will be clear to those skilled in the art from the succeeding detailed description of the preferred embodiment of the invention and the accompanying drawings thereof.
FIG. 1 is a sectional view of a rotary regenerator taken in a plane containing the axis of rotation thereof.
FIG. 2 is a fragmentary elevation view of one face of a matrix, with parts cut away.
FIG. 3 is a fragmentary enlargement of FIG. 1.
FIG. 4 is a fragmentary axonometric view of a matrix.
Referring first to FIG. 1, a gas turbine engine may include an engine block or housing 9 which supports the rotating parts and combustion chamber of the engine (not illustrated) and which also supports a rotary regenerator R including an axial-flow matrix 10. The matrix is mounted for rotation about a horizontal axis, as illustrated, at a side face of the block 9. The matrix is enclosed by the block 9 and a regenerator cover 11 fixed to the block, these two constituting a housing for the matrix. The regenerator cover defines a cool air inlet 13 and an exhaust outlet 14. The block 9 defines a hot air outlet 15 opposite to the inlet 13 and a hot gas inlet 17 opposite to the exhaust outlet 14.
The matrix 10 is of known type embodying a hub or inner ring 18 by which it is driven, an annulus 19 of heat exchange material defining passages extending generally parallel to the axis from face to face of the matrix, and an outer ring or outer rim 20. The heat exchange material 19 is fixed to the hub 18. Seals cooperating with the matrix include an outer side rim seal 23 engaging the matrix adjacent the rim, an outer side hub seal 24 engaging the hub, an inner side rim seal 25 opposite to (Pat. No. 3,476,173) are seal 23, and an inner side hub seal 26 opposite to seal 24.
The sealing structure also includes radial crossarm seals extending from the hub to the outer margin of the matrix (not illustrated) to block flow from one fluid passage to the other across the face of the matrix. These seals may be as described in Pat. No. 3,368,611.
The means for driving and supporting the matrix illustrated is the same as one form shown in the prior application referred to above. It includes a shaft 30 rotatably mounted in the housing driven by a sprocket 31. An inner coupling member 34 fixed on the shaft is coupled by a flexible connection to an outer coupling member 35 which connects the shaft to the hub 18 of the matrix.
The sheet metal matrix is of such a nature as to provide numerous small passages or pores 37 extending parallel to the axis of the matrix. Generally speaking, this structure is made by laying up alternate spirals 39 of flat sheet metal and 40 of corrugated sheet metal, which are then bonded together by brazing.
The means for blocking transmission of pressure from face to face of the matrix through the marginal part engaged by the rim seals is shown particularly in FIGS. 3 and 4. The radially outer portion 50 of the matrix between seals such as 23 and 25 embodies alternating flat sheets 51 and corrugated sheets 53. The corrugated sheets may be similar to those in the main portion 19 3 of the matrix but, in general, the corrugations in the blocked outer portion are shallow while those in the inner portion may not be.
To block flow through the passages 55 which would otherwise be defined between the fiat and corrugated sheets, the corrugated sheets 53 are provided with two ridges or corrugations 57 and 58 extending lengthwise of the corrugated strip and circumferentially of the matrix, crossing the normal corrugations of the strip which extend axially of the matrix. The circumferential 1y extending ridges 57 and 58, as can clearly be seen, out off or block the passages which otherwise would exist between adjacent flat sheets 51. When the assembly of the matrix is completed, the peaks of outward extending ridge 58 bear tightly against and are brazed to the next adjacent fiat sheet 51 outward of the corrugated sheet and the peaks of corrugations of ridge 57 similarly bear against the next inner flat sheet 51. Thus, the two ridges block the otherwise existing flow passages on both the outer and inner sides of the corrugated sheet 53.
The ridges 57 and 58 may be provided during the rolling to provide the normal corrugations of the sheet or may be added by a subsequent rolling operation.
Precise control of the action of the seal and accurate response of the seal engaging force to the varying pressures which may exist in different conditions of regenerator operation are assured by presence of the barrier defined by ridges 57 and 58.
The detailed description of the preferred embodiment of our invention for the purpose of explaining the principles thereof is not to be considered as limiting or re stricting the invention, since many modifications may be made by the exercise of skill in the art without departing from the scope of the invention.
What is claimed is:
1. A rotary regenerator comprising, in combination, a housing, an axial-flow matrix having radial faces and an outer circumferential surface, the matrix including heat-exchange material defining multifarious distinct generally parallel passages from face to face of the matrix, means mounting the matrix rotatably in the housing, and seal means mounted on the housing engaging at least one face of the matrix adjacent the outer surface of the matrix; the matrix including a peripheral annular zone cooperating with the said seal means, the said peripheral zone comprising alternating smooth and corrugated metal strips with the corrugated strips spacing the metal strips and defining passages across the matrix, the corrugated strips in the said zone having oppositely directed circumferential ridges blocking the said passages so as to isolate the matrix-engaging surface of the seal means from exposure to pressure communicated through the matrix from the remote face of the matrix.
2. A regenerator as recited in claim 1 in which the ridges are spaced inwardly from the faces of the matrix.
References Cited UNITED STATES PATENTS 3,392,776 7/1968 Topouzian l10X ROBERT A. OLEARY, Primary Examiner A. W. DAVIS, JR., Assistant Examiner US. Cl. X,R. l()
US777264A 1968-11-20 1968-11-20 Rotary regenerator Expired - Lifetime US3511309A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3901309A (en) * 1974-05-16 1975-08-26 Gen Motors Corp Regenerator disk flexible rim
US3939904A (en) * 1972-10-25 1976-02-24 Beaufrere Albert H Rotary disc regenerator
US4306611A (en) * 1980-08-28 1981-12-22 Corning Glass Works Rotary heat exchanger

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3392776A (en) * 1966-11-03 1968-07-16 Ford Motor Co Spirally wound rotary heat exchanger having barrel center mount

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3392776A (en) * 1966-11-03 1968-07-16 Ford Motor Co Spirally wound rotary heat exchanger having barrel center mount

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3939904A (en) * 1972-10-25 1976-02-24 Beaufrere Albert H Rotary disc regenerator
US3901309A (en) * 1974-05-16 1975-08-26 Gen Motors Corp Regenerator disk flexible rim
US4306611A (en) * 1980-08-28 1981-12-22 Corning Glass Works Rotary heat exchanger

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