US3255818A - Involute plate heat exchanger - Google Patents

Involute plate heat exchanger Download PDF

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US3255818A
US3255818A US350283A US35028364A US3255818A US 3255818 A US3255818 A US 3255818A US 350283 A US350283 A US 350283A US 35028364 A US35028364 A US 35028364A US 3255818 A US3255818 A US 3255818A
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casing
passages
heat exchanger
manifolds
plates
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US350283A
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Jr Paul E Beam
Jr Esten W Spears
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Motors Liquidation Co
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Motors Liquidation Co
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Priority to US350283A priority Critical patent/US3255818A/en
Priority to GB8127/65A priority patent/GB1027210A/en
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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
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/04Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being formed by spirally-wound plates or laminae
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G5/00Profiting from waste heat of combustion engines, not otherwise provided for
    • F02G5/02Profiting from waste heat of exhaust gases
    • 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
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0012Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the apparatus having an annular form
    • F28D9/0018Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the apparatus having an annular form without any annular circulation of the heat exchange media
    • 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
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies
    • 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
    • Y10S165/355Heat exchange having separate flow passage for two distinct fluids
    • Y10S165/356Plural plates forming a stack providing flow passages therein
    • Y10S165/357Plural plates forming a stack providing flow passages therein forming annular heat exchanger
    • Y10S165/358Radially arranged plates

Definitions

  • This invention relates to heat exchangers and more particularly to toroidal heat exchangers for transferring heat from one fluid to another and especially adapted for heating combustion air for aircraft engine use by extracting heat from engine exhaust gases.
  • each heat exchanger annular in form it is particularly advantageous to make each heat exchanger annular in form and when this is done difiiculties are encountered in compensating for variations in fluid pressure drop'and heat transfer characteristics within the cross sectional area from the inside to the outside diameter of the heat exchanger in achieving efficiency.
  • An object of the present invention is to provide an improved annular or toroidal heat exchanger of maximum efficiency and of simple plate construction.
  • a feature of the present invention pertains to a heat exchanger comprising an annular casingand a cylindrical casing joined by an interposed toroidal heat exchange means or core formed with involute plates such that the flow of fluids through the heat exchanger in the general direction of its axis may be at a more uniform rate across the cross sectional area of the core to promote maximum heat exchange efficiency.
  • FIGURE 1 is an elevation view of a combustion air duct with portions removed and showing, in longitudinal section, a heat exchanger of the present invention installed for' cooperation with the duct in extracting heat from engine combustion gases;
  • FIGURE 2 is a sectional view looking in the direction of the arrows 2-2 in FIGURE 1;
  • FIGURE 3 is a perspective view of the duct and heat exchanger of FIGURE 1 with parts broken away better to illustrate the construction;
  • FIGURE 4 is an exploded view of two adjacent corrugated sections each in involute form and as utilized in the heat exchanger of FIGURES 1 to 3.
  • the heat exchanger of the drawings comprises an inner cylindrical casing or flow divider and an outer annular casing 12 having a common axis.
  • Two toroidal manifolds 14 and 16 are provided each being at one end of the outer annular casing 12 and communicating with a toroidal multi-plate heat exchange means or core generally indicated at 18.
  • the latter bridges the annular space between the casings 10 and 12 and is formulated of a series of consecutive sets of four involute plates 20, 22 and 24 and 26.
  • Each plate 20 cooperates with a plate 24 to enclose a corrugated plate 22 and also cooperates with another plate 24 on its other side to confine a corrugated plate 26.
  • the outer ends of the plates 20 and 24 of each set are joined at their margins as best illustrated in FIGURE 2 closely to approach the inside wall surface of the outer annular casing 12.
  • the plates 20 and 24 are smooth surfaced, i.e. not corrugated.
  • FIGURE 2 also shows how the corrugated and smooth surfaced plates are nested together with inner margins 25 of the plates 24 in close contact with the outer wall of the inner cylindrical casing 10 and margins of the plates 20 resting on the margins 25 of the plates 24. Variations in the design of these details are possible without departing from the present invention.
  • the manifold 14 is served by means of an inlet conduit 30 and the manifold 16 is served by means of anoutlet conduit 32.
  • the nested or annularly stacked plates of the heat exchange means'or core 18 are so formed as to define two alternate sets of passages extending parallel with the axis of the heat exchanger.
  • the passages A of one of these sets provide connections or heated fluid communication between the manifolds 14 and 16 but are otherwise closed by wall portions 33 made from the plates 20.
  • the passages of the other of the sets provide connections through the heat exchanger means 18 for handling cooler fluid flowing through a conduit 34 in paths parallel with the axis of the heat exchanger.
  • the casing 12 includes two end rings 36 and 38 as well as two annular and frustoconical plates 40 and 42.
  • the end plates 36 and 38 merely serve as convenient connecting plates between the manifolds 16 and 14 and the conduit 34 whereas the plates 40 and 42 are apertured as at 44 properly to connect the manifolds with the alternate passages A of the heat exchange means 18.
  • passages B Alternating with the passages A are passages B and these passages B are each defined between adjacent plates 20 and 24 to handle the cooler fluid of the conduit 34.
  • the passages A each enclose a corrugated plate 26 which progressively narrows in width toward the heat exchanger 1 axis whereas each of the passages B encloses a corrugated plate 22 which progressively increases in width toward that axis, these widths being measured in a direction parallel with the heat exchange axis.
  • a narrow width places less restriction on fluid flow than is done by a greater width and this fact is availed of to achieve uniform flow rates regardless of at which radius each rate is measured for either of both fluids being handled.
  • a hot gas or fluid entering at 30 and distributed by the manifold 14 will flow through the passages A and will tend to flow along all the grooves of each of the corrugated plates 26 despite the fact that the gas is admitted and discharged near the outer periphery of the heat exchanger core.
  • the air or other fluid to be heated passing countercurrent to the first fluid and along the conduit 34 will flow along all the grooves in each of the corrugated plates 22 although that other fluid is admitted and discharged adjacent the inner periphery of the heat exchanger means or core 18.
  • the corrugated plates 22 and 26 not only make the flow rate of each gas more uniform throughout the cross-sectional area of the heat exchanger means but also contribute to a more intimate heat transfer relation between the fluids.
  • a heat exchanger comprising an inner cylindrical casing and an outer annular casing, said casings having a common axis, two toroidal manifolds, one of said manifolds being positioned at each end of said outer annular casing, toroidal heat exchange means comprising an annular series of involute plates bridging the space between said casings and defining passages with each passage extending radially and outwardly from said inner casing to said outer casing and between said manifolds, alternating passages as defined by said plates connecting said manifolds and conducting one fluid, the remainder of the passages forming paths parallel to said common axis for conducting a second fluid therethrough, a corrugated involute plate in each of said passages having its width measured in the direction of the heat exchanger axis, each corrugated plate in said alternating passages progressively increasing in width from said inner casing to said outer casing and each corrugated plate in the remaining passages progressively decreasing in width from said inner casing to said outer casing so as to

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

Description

June 14, 1966 p. E. BEAM, JR., ETAL 3,255,818
INVOLUTE PLATE HEAT EXCHANGER Filed March 9, 1964 2 Sheets-Sheet l /0 INVENTORS 5 011! 5 ee/v; (/1 24? BY 55k Z15 army/1 wye A ORNE) June 14, 1966 P. E. BEAM, JR., ETAL 3,255,818
Filed March 9, 1964 5 J m m mm m m m3 Y ATTORNEY United States Patent 3,255,818 INVOLUTE PLATE HEAT EXCHANGER Paul E. Beam, Jr., and Esten W. Spears, Jr., Indianapolis, Ind., assignors to General Motors Corporation, Detroit, Mich, a corporation of Delaware Filed Mar. 9, 1964, Ser. No. 350,283 2 Claims. (Cl. 165-166) This invention relates to heat exchangers and more particularly to toroidal heat exchangers for transferring heat from one fluid to another and especially adapted for heating combustion air for aircraft engine use by extracting heat from engine exhaust gases.
With regard to heat exchangers of the type herein considered, it is particularly advantageous to make each heat exchanger annular in form and when this is done difiiculties are encountered in compensating for variations in fluid pressure drop'and heat transfer characteristics within the cross sectional area from the inside to the outside diameter of the heat exchanger in achieving efficiency.
An object of the present invention is to provide an improved annular or toroidal heat exchanger of maximum efficiency and of simple plate construction.
A feature of the present invention pertains to a heat exchanger comprising an annular casingand a cylindrical casing joined by an interposed toroidal heat exchange means or core formed with involute plates such that the flow of fluids through the heat exchanger in the general direction of its axis may be at a more uniform rate across the cross sectional area of the core to promote maximum heat exchange efficiency.
These and other important features of the invention will now be described in detail in the specification and then pointed out more particularly in the appended claims.
In the drawings:
FIGURE 1 is an elevation view of a combustion air duct with portions removed and showing, in longitudinal section, a heat exchanger of the present invention installed for' cooperation with the duct in extracting heat from engine combustion gases;
FIGURE 2 is a sectional view looking in the direction of the arrows 2-2 in FIGURE 1;
FIGURE 3 is a perspective view of the duct and heat exchanger of FIGURE 1 with parts broken away better to illustrate the construction; and
FIGURE 4 is an exploded view of two adjacent corrugated sections each in involute form and as utilized in the heat exchanger of FIGURES 1 to 3.
The heat exchanger of the drawings comprises an inner cylindrical casing or flow divider and an outer annular casing 12 having a common axis. Two toroidal manifolds 14 and 16 are provided each being at one end of the outer annular casing 12 and communicating with a toroidal multi-plate heat exchange means or core generally indicated at 18. The latter bridges the annular space between the casings 10 and 12 and is formulated of a series of consecutive sets of four involute plates 20, 22 and 24 and 26. Each plate 20 cooperates with a plate 24 to enclose a corrugated plate 22 and also cooperates with another plate 24 on its other side to confine a corrugated plate 26. The outer ends of the plates 20 and 24 of each set are joined at their margins as best illustrated in FIGURE 2 closely to approach the inside wall surface of the outer annular casing 12. The plates 20 and 24 are smooth surfaced, i.e. not corrugated.
FIGURE 2 also shows how the corrugated and smooth surfaced plates are nested together with inner margins 25 of the plates 24 in close contact with the outer wall of the inner cylindrical casing 10 and margins of the plates 20 resting on the margins 25 of the plates 24. Variations in the design of these details are possible without departing from the present invention.
Patented June 14, 1966 In the disclosure of FIGURE 1, the manifold 14 is served by means of an inlet conduit 30 and the manifold 16 is served by means of anoutlet conduit 32. The nested or annularly stacked plates of the heat exchange means'or core 18 are so formed as to define two alternate sets of passages extending parallel with the axis of the heat exchanger. The passages A of one of these sets provide connections or heated fluid communication between the manifolds 14 and 16 but are otherwise closed by wall portions 33 made from the plates 20. The passages of the other of the sets provide connections through the heat exchanger means 18 for handling cooler fluid flowing through a conduit 34 in paths parallel with the axis of the heat exchanger. The casing 12 includes two end rings 36 and 38 as well as two annular and frustoconical plates 40 and 42. The end plates 36 and 38 merely serve as convenient connecting plates between the manifolds 16 and 14 and the conduit 34 whereas the plates 40 and 42 are apertured as at 44 properly to connect the manifolds with the alternate passages A of the heat exchange means 18.
Alternating with the passages A are passages B and these passages B are each defined between adjacent plates 20 and 24 to handle the cooler fluid of the conduit 34. The passages A each enclose a corrugated plate 26 which progressively narrows in width toward the heat exchanger 1 axis whereas each of the passages B encloses a corrugated plate 22 which progressively increases in width toward that axis, these widths being measured in a direction parallel with the heat exchange axis. A narrow width places less restriction on fluid flow than is done by a greater width and this fact is availed of to achieve uniform flow rates regardless of at which radius each rate is measured for either of both fluids being handled.
A hot gas or fluid entering at 30 and distributed by the manifold 14 will flow through the passages A and will tend to flow along all the grooves of each of the corrugated plates 26 despite the fact that the gas is admitted and discharged near the outer periphery of the heat exchanger core. The air or other fluid to be heated passing countercurrent to the first fluid and along the conduit 34 will flow along all the grooves in each of the corrugated plates 22 although that other fluid is admitted and discharged adjacent the inner periphery of the heat exchanger means or core 18. The corrugated plates 22 and 26 not only make the flow rate of each gas more uniform throughout the cross-sectional area of the heat exchanger means but also contribute to a more intimate heat transfer relation between the fluids.
We claim:
1. A heat exchanger comprising an inner cylindrical casing and an outer annular casing, said casings having a common axis, two toroidal manifolds, one of said manifolds being positioned at each end of said outer annular casing, toroidal heat exchange means comprising an annular series of involute plates bridging the space between said casings and defining passages with each passage extending radially and outwardly from said inner casing to said outer casing and between said manifolds, alternating passages as defined by said plates connecting said manifolds and conducting one fluid, the remainder of the passages forming paths parallel to said common axis for conducting a second fluid therethrough, a corrugated involute plate in each of said passages having its width measured in the direction of the heat exchanger axis, each corrugated plate in said alternating passages progressively increasing in width from said inner casing to said outer casing and each corrugated plate in the remaining passages progressively decreasing in width from said inner casing to said outer casing so as to effect uniformity of flow rate of the fluid flowing along opposite surfaces of the corrugated involute plates.
3 2. A heat exchanger as set forth in claim 1 wherein said outer annular casing includes a pair of frusto-conical plates having apertures for communicating said one fluid between said toroidal manifolds and said alternating passages.
References Cited by the Examiner UNITED STATES PATENTS 721,310 2/1903 Junkers 165-161 2,354,698 8/1944 Morris 165166 2,516,910 8/1950 Redding 6039.51 X 2,646,027 7/1953 Ackerman et al. 165166 X 3,098,522 7/1963 McCormick 165166 3,166,122 1/1965 Hryniszak 165166 X FOREIGN PATENTS 5 276,761 4/ 1927 Great Britain. 581,742 10/ 1946 Great Britain.
ROBERT A. OLEARY, Primary Examiner.
10 CHARLES SUKALO, Examiner.
T. W. STREULE, Assistant Examiner.

Claims (1)

1. A HEAT EXCHANGER COMPRISING AN INNER CYLINDRICAL CASING AND AN OUTER ANNULAR CASING, SAID CASINGS HAVING A COMMON AXIS, TWO TOROIDAL MANIFOLDS, ONE OF SAID MANIFOLDS BEING POSITIONED AT EACH END OF SAID OUTER ANNULAR CASING, TOROIDAL HEAT EXCHANGE MEANS COMPRISING AN ANNULAR SERIES OF INVOLUTE PLATES BRIDGING THE SPACE BETWEEN SAID CASINGS AND DEFINING PASSAGES WITH EACH PASSAGE EXTENDING RADIALLY AND OUTWARDLY FROM SAID INNER CASING TO SAID OUTER CASING AND BETWEEN SAID MANIFOLDS, ALTERNATING PASSAGES AS DEFINED BY SAID PLATES CONNECTING SAID MANIFOLDS AND CONDUCTING ONE FLUID, THE REMAINDER OF THE PASSAGES FORMING PATHS PARALLEL TO SAID COMMON AXIS FOR CONDUCTING A SECOND FLUID THERETHROUGH, A CORRUGATED INVOLUTE PLATE IN EACH OF SAID PASSAGES HAVING ITS WIDTH MEASURED IN THE DIRECTION OF THE HEAT EXCHANGER AXIS, EACH CORRUGATED PLATE IN SAID ALTERNATING PASSAGES PROGRESSIVELY INCREASING IN WIDTH FROM SAID INNER CASING TO SAID OUTER CASING AND EACH CORRUGATED PLATE IN THE REMAINING PASSAGES PROGRESSIVELY DECREASING IN WIDTH FROM SAID INNER CASING TO SAID OUTER CASING SO AS TO EFFECT UNIFORMITY OF FLOW RATE OF THE FLUID FLOWING ALONG OPPOSITE SURFACES OF THE CORRUGATED INVOLUTE PLATES.
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Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3507115A (en) * 1967-07-28 1970-04-21 Int Harvester Co Recuperative heat exchanger for gas turbines
DE2321378A1 (en) 1972-04-29 1973-11-08 Getters Spa CATALYST CARTRIDGE
DE2721321A1 (en) * 1976-07-30 1978-02-02 Sulzer Ag HEAT TRANSFER WITH A WALL-LIKE SEPARATION FOR THE TWO MEDIA INVOLVED IN THE HEAT TRANSFER
US4098330A (en) * 1976-07-23 1978-07-04 General Motors Corporation Annular metal recuperator
US4475586A (en) * 1979-02-28 1984-10-09 Mtu Motoren-Und Turbinen Union Munchen Gmbh Heat exchanger
US5060721A (en) * 1990-05-29 1991-10-29 Solar Turbines Incorporated Circular heat exchanger
US5065816A (en) * 1990-05-29 1991-11-19 Solar Turbines Incorporated Sealing system for a circular heat exchanger
WO1991019151A1 (en) * 1990-05-29 1991-12-12 Solar Turbines Incorporated Circular heat exchanger having uniform cross-sectional area throughout the passages therein
US5082050A (en) * 1990-05-29 1992-01-21 Solar Turbines Incorporated Thermal restraint system for a circular heat exchanger
US5878590A (en) * 1998-02-25 1999-03-09 General Motors Corporation Dehumidifying mechanism for auto air conditioner with improved space utilization and thermal efficiency
US6357113B1 (en) 1999-11-04 2002-03-19 Williams International Co., L.L.C. Method of manufacture of a gas turbine engine recuperator
US6438936B1 (en) 2000-05-16 2002-08-27 Elliott Energy Systems, Inc. Recuperator for use with turbine/turbo-alternator
US20030131978A1 (en) * 2001-11-30 2003-07-17 Toyo Radiator Co., Ltd. Cylinder-type heat exchanger
US20070137844A1 (en) * 2005-12-02 2007-06-21 Herbert Aigner Plate heat exchanger
US20120216544A1 (en) * 2011-02-28 2012-08-30 Andreas Eleftheriou Swirl reducing gas turbine engine recuperator
US20170198974A1 (en) * 2016-01-08 2017-07-13 General Electric Company Heat Exchanger for Embedded Engine Applications
US20170198637A1 (en) * 2016-01-08 2017-07-13 General Electric Company Heat Exchanger for Embedded Engine Applications: Transduct Segments
US20170350655A1 (en) * 2014-12-18 2017-12-07 Maico Elektroapparate-Fabrik Gmbh Heat exchanger and air device having said heat exchanger
EP3321622A3 (en) * 2016-08-22 2018-08-01 United Technologies Corporation Panel based heat exchanger
US10914532B2 (en) * 2015-09-04 2021-02-09 Kyungdong Navien Co., Ltd. Curved plate heat exchanger
US11441850B2 (en) * 2020-01-24 2022-09-13 Hamilton Sundstrand Corporation Integral mounting arm for heat exchanger
US11453160B2 (en) 2020-01-24 2022-09-27 Hamilton Sundstrand Corporation Method of building a heat exchanger
US11460252B2 (en) 2020-01-24 2022-10-04 Hamilton Sundstrand Corporation Header arrangement for additively manufactured heat exchanger
US11703283B2 (en) 2020-01-24 2023-07-18 Hamilton Sundstrand Corporation Radial configuration for heat exchanger core

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US721310A (en) * 1902-01-20 1903-02-24 Hugo Junkers Surface condenser.
GB276761A (en) * 1926-06-14 1927-09-08 George Edward Tansley Improvements in or relating to air or water heaters and dust separators used in connection with furnaces
US2354698A (en) * 1942-03-06 1944-08-01 Gen Electric Gas turbine
GB581742A (en) * 1943-04-27 1946-10-23 Bristol Aeroplane Co Ltd Improvements in or relating to heat-exchangers
US2516910A (en) * 1948-06-02 1950-08-01 Westinghouse Electric Corp Gas turbine apparatus with selective regenerator control
US2646027A (en) * 1951-02-28 1953-07-21 Curtiss Wright Corp Aftercooler construction
US3098522A (en) * 1959-08-07 1963-07-23 Gen Motors Corp Stacked plate heat exchangers
US3166121A (en) * 1961-01-27 1965-01-19 Svenska Flaektfabriken Ab Space heat exchange unit

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US721310A (en) * 1902-01-20 1903-02-24 Hugo Junkers Surface condenser.
GB276761A (en) * 1926-06-14 1927-09-08 George Edward Tansley Improvements in or relating to air or water heaters and dust separators used in connection with furnaces
US2354698A (en) * 1942-03-06 1944-08-01 Gen Electric Gas turbine
GB581742A (en) * 1943-04-27 1946-10-23 Bristol Aeroplane Co Ltd Improvements in or relating to heat-exchangers
US2516910A (en) * 1948-06-02 1950-08-01 Westinghouse Electric Corp Gas turbine apparatus with selective regenerator control
US2646027A (en) * 1951-02-28 1953-07-21 Curtiss Wright Corp Aftercooler construction
US3098522A (en) * 1959-08-07 1963-07-23 Gen Motors Corp Stacked plate heat exchangers
US3166121A (en) * 1961-01-27 1965-01-19 Svenska Flaektfabriken Ab Space heat exchange unit

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3507115A (en) * 1967-07-28 1970-04-21 Int Harvester Co Recuperative heat exchanger for gas turbines
DE2321378A1 (en) 1972-04-29 1973-11-08 Getters Spa CATALYST CARTRIDGE
DE2366546C2 (en) * 1972-04-29 1988-12-22 Saes Getters S.P.A., Mailand/Milano Heat exchanger
US4098330A (en) * 1976-07-23 1978-07-04 General Motors Corporation Annular metal recuperator
DE2721321A1 (en) * 1976-07-30 1978-02-02 Sulzer Ag HEAT TRANSFER WITH A WALL-LIKE SEPARATION FOR THE TWO MEDIA INVOLVED IN THE HEAT TRANSFER
US4475586A (en) * 1979-02-28 1984-10-09 Mtu Motoren-Und Turbinen Union Munchen Gmbh Heat exchanger
WO1991019151A1 (en) * 1990-05-29 1991-12-12 Solar Turbines Incorporated Circular heat exchanger having uniform cross-sectional area throughout the passages therein
US5065816A (en) * 1990-05-29 1991-11-19 Solar Turbines Incorporated Sealing system for a circular heat exchanger
US5060721A (en) * 1990-05-29 1991-10-29 Solar Turbines Incorporated Circular heat exchanger
US5082050A (en) * 1990-05-29 1992-01-21 Solar Turbines Incorporated Thermal restraint system for a circular heat exchanger
US5081834A (en) * 1990-05-29 1992-01-21 Solar Turbines Incorporated Circular heat exchanger having uniform cross-sectional area throughout the passages therein
US5878590A (en) * 1998-02-25 1999-03-09 General Motors Corporation Dehumidifying mechanism for auto air conditioner with improved space utilization and thermal efficiency
USRE38181E1 (en) 1998-02-25 2003-07-15 Delphi Technologies, Inc. Dehumidifying mechanism for auto air conditioner with improved space utilization and thermal efficiency
US6357113B1 (en) 1999-11-04 2002-03-19 Williams International Co., L.L.C. Method of manufacture of a gas turbine engine recuperator
US6438936B1 (en) 2000-05-16 2002-08-27 Elliott Energy Systems, Inc. Recuperator for use with turbine/turbo-alternator
US6837419B2 (en) 2000-05-16 2005-01-04 Elliott Energy Systems, Inc. Recuperator for use with turbine/turbo-alternator
US20030131978A1 (en) * 2001-11-30 2003-07-17 Toyo Radiator Co., Ltd. Cylinder-type heat exchanger
US6789616B2 (en) * 2001-11-30 2004-09-14 Toyo Radiator Co., Ltd. Cylinder-type heat exchanger
US20070137844A1 (en) * 2005-12-02 2007-06-21 Herbert Aigner Plate heat exchanger
US20120216544A1 (en) * 2011-02-28 2012-08-30 Andreas Eleftheriou Swirl reducing gas turbine engine recuperator
US9766019B2 (en) * 2011-02-28 2017-09-19 Pratt & Whitney Canada Corp. Swirl reducing gas turbine engine recuperator
US20170350655A1 (en) * 2014-12-18 2017-12-07 Maico Elektroapparate-Fabrik Gmbh Heat exchanger and air device having said heat exchanger
US11486649B2 (en) * 2014-12-18 2022-11-01 Maico Elektroapparate-Fabrik Gmbh Cylindrical air to air heat exchanger
US10914532B2 (en) * 2015-09-04 2021-02-09 Kyungdong Navien Co., Ltd. Curved plate heat exchanger
CN106959034B (en) * 2016-01-08 2019-06-18 通用电气公司 Heat exchanger for embedded engine application
US10126062B2 (en) * 2016-01-08 2018-11-13 General Electric Company Heat exchanger for embedded engine applications
CN106959034A (en) * 2016-01-08 2017-07-18 通用电气公司 Heat exchanger for embedded engine application
US10344674B2 (en) * 2016-01-08 2019-07-09 General Electric Company Heat exchanger for embedded engine applications: transduct segments
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US11441850B2 (en) * 2020-01-24 2022-09-13 Hamilton Sundstrand Corporation Integral mounting arm for heat exchanger
US11453160B2 (en) 2020-01-24 2022-09-27 Hamilton Sundstrand Corporation Method of building a heat exchanger
US11460252B2 (en) 2020-01-24 2022-10-04 Hamilton Sundstrand Corporation Header arrangement for additively manufactured heat exchanger
US11703283B2 (en) 2020-01-24 2023-07-18 Hamilton Sundstrand Corporation Radial configuration for heat exchanger core
US11752691B2 (en) 2020-01-24 2023-09-12 Hamilton Sundstrand Corporation Method of building a heat exchanger

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