US2952445A - Damage resistant plate type heat exchanger - Google Patents

Damage resistant plate type heat exchanger Download PDF

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US2952445A
US2952445A US744607A US74460758A US2952445A US 2952445 A US2952445 A US 2952445A US 744607 A US744607 A US 744607A US 74460758 A US74460758 A US 74460758A US 2952445 A US2952445 A US 2952445A
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plates
fin
heat exchanger
plate type
exchanger
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US744607A
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Edward L Ladd
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United Aircraft Products Inc
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United Aircraft Products Inc
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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
    • F28D9/0062Heat-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 for one heat-exchange medium being formed by spaced plates with inserted elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/02Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
    • F28F3/025Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being corrugated, plate-like elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2215/00Fins
    • F28F2215/04Assemblies of fins having different features, e.g. with different fin densities
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2265/00Safety or protection arrangements; Arrangements for preventing malfunction
    • 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
    • Y10S165/387Plural plates forming a stack providing flow passages therein including side-edge seal or edge spacer bar
    • Y10S165/39Flange element to connect two adjacent heat exchange plates

Definitions

  • Plate type exchangers commonly are comprised of a plurality of superposed spaced apart plates closed at selected marginal edges to define alternate fluid flowing ducts for different fluids to be brought into heat transfer relation, the exchange of heat taking place between adjacent ducts through a separating plate.
  • corrugated fin material is placed within the ducts to aid in the absorption and transfer of heat.
  • the exchanger For aircraft use, where weight conservation is necessarily a prime objective, it is customary to construct the exchanger of light weight metals such as a aluminum alloys.
  • the plates are made thin and the fin material is formed of still thinner, ductile sheet metal. So fabricated, an exchanger is effectively reduced in weight but other problems are introduced such as the obtaining of an inexpensive, secure means of uniting the component parts of the exchanger.
  • the instant invention has in view a concept of a light weight heat exchanger specially constructed for operation under high pressures and for resistance to air flow damage as described.
  • Features of such concept lie in a new means of fabrication wherein the fin material serves the dual purpose of more effectively transferring heat and of acting as tie strips positively to connect adjacent plates to one another.
  • an all brazed construction is contemplated obviating the need for separable connecting devices, and, still further, a generally new fin structure is proposed characterized by the use of a relatively short length fin at the entrance end of the duct made of a heat treatable, damage resistant material and spaced from following fin material in a manner to define therewith a plenum chamber for lateral distribution of the flowing fluid.
  • Fig. 1 is a fragmentary view of a plate type heat exchanger in accordance with the illustrated embodiment of the invention, shown in a longitudinal section taken substantially along the line 11 of Fig. 2;
  • Fig. 2 is a view in cross section taken substantially along the line 2-2 of Fig. 1;
  • Fig. 3 is a view in top longitudinal section, taken substantially along the line 33 of Fig. l;
  • Fig. 4 is a view in perspective of the portion of the illustrative heat exchanger shown in Figs. 1 to 3.
  • a heat exchanger in accordice ance with the illustrated embodiment of the invention comprises a series of stacked plates of a number selected in accordance with the number of fluid passes or fluid flowing ducts to be provided by the exchanger.
  • four plates, 1, 2, 3 and 4 are shown. These plates have substantially the same configuration and are made of a thin light weight metal.
  • the plates 1 and 2 are held spaced apart by marginal strips 5. Similar strips 6 hold the plates 3 and 4 in spaced relation and there is interposed between the plates 2 and 3 strip fins 7 and 8, there being further disposed between the plates 2 and 3 marginal strips 9 (one shown) as seen in Fig. 4.
  • the fins 7 and 8 are spaced apart and define between them a plenum chamber 10.
  • the arrangement is one devised to bring two fluids into heat transfer relation through separating plates.
  • the marginal pieces 9 close opposite side edges of adjacent plates 2 and 3 and define therewith a fluid flowing duct open at its opposite ends for flow therethrough as indicated by the arrows in Fig. 1.
  • the marginal pieces 5 are disposed at right angles to the pieces 9 and define with the plates 1 and 2 a duct for flow at right angles to the direction of flow in the space between plates 2 and 3.
  • the marginal pieces 6 are arranged like the pieces 5.
  • the upper and lower ducts as described may communicate with a common header 11 to receive a fluid flow.
  • the header 11 and its communicating ducts constitute a part of a closed fluid flowing system, for example a lubricant circulating system.
  • the duct for flow of the first fluid is open to ambient air flow.
  • the exchanger In the installation of the exchanger it is placed in an air duct or the like with the ram force of the moving air applied to that face of the exchanger offering open passes through the plates 2 and 3.
  • the arrangement of the fins 7 and 8- is such as to present the longitudinal edges thereof to such air flow, the air flowing lengthwise along the fins which are corrugated to define in effect a plurality of separated longitudinal passes through the duct of the exchanger.
  • the alternate hills and valleys of the fin are respectively in contact With the plates 2 and 3 to close off such individual passes and with the further eflect aiding in a more thorough absorption of heat from or into the flowing fluid.
  • the fin 7 is short in length relatively to the fin 8 and is made of a heat treatable material in order that it can be hardened and made resistant to abrasion and impact damage from particles in the flowing air stream.
  • the heat exchanger presents a hard, relatively unyielding face to the ram air there being presented only the edges of plates 1, 2, 3 and 4, the marginal pieces 5 and 6 and the edges of the fin 7.
  • the marginal pieces 5 and 6 may also be hardened as the fin 7 so that the entire face of the exchanger is made damage resistant.
  • the separation of the fin means 78 into two parts reduces the cost of the assembly inasmuch as the major portion of the fin means is represented by the fin 8 which may be made of the conventional untreated aluminum alloy.
  • the fins are made of a thin and ductile material corrugated or crimped to the configuration shown and placed between adjacent plates of the heat exchanger with side edges of the fin strip in contact with the marginal closure pieces, the strip being in effect confined along its side edges by such marginal pieces,
  • a plate type heat exchanger constructed for weight conservation and damage resistance, including a pair of spaced apart thin metal plates of four side configuration and aligned in superposed relation to one another, closure means received between opposing side edges of said plates and defining with said platesa fluid flowing duct having opposed open entrance and exit ends, strip fin means installed in said duct including first and second strip fins made of foil-like sheet metal material of the same gauge and heat transfer capabilities and crirnped to present alternate hills and valleys in contact respectively with the opposing surfaces of said plates, one of said strip fins being relatively shorter in length than the other and made of heat treatable material and further being stationed at the entrance end of the duct ahead of the other fin, said other fin being, spaced from said one fin a distance corresponding to a substantial part of the length of said one fin to define intermediate the fins a plenum chamber for lateral distribution of fluid and said other fin extending uninterruptedly throughout the remaining length of said duct to said exit end thereof, and means uniting the assembly comprising said plates, said closures and said fins
  • a plate type heat exchanger characterized by additional thin metal plates above and below said pair of plates, and closures installed in opposing side edges of adjacent plates above and below said pair of plates to. define other fluid flowing ducts in transverse relation to the first said fluid flowing duct, the last said closures being made of heat treatable material to present in conjunction with said one strip fin a damage resistant face on one side of the heat exchanger.

Description

Sept. 13, 1960 E. L. LADD 2,952,445
DAMAGE RESISTANT PLATE TYPE HEAT EXCHANGER Filed June 25, 1958 V o" I 1 f I H H m H do ATTORNE? United States Patent DAMAGE RESISTANT PLATE TYPE HEAT EXCHANGER Edward L. Ladd, Dayton, Ohio, assignor to United Aircraft Products, Inc., Dayton, Ohio, a corporation of Ohio Filed June 25, 1958, Ser. No. 744,607
2 Claims. (Cl. 257-245) This invention relates to heat transfer equipment and particularly to plate type exchangers constructed with a view to maximum weight conservation.
Plate type exchangers commonly are comprised of a plurality of superposed spaced apart plates closed at selected marginal edges to define alternate fluid flowing ducts for different fluids to be brought into heat transfer relation, the exchange of heat taking place between adjacent ducts through a separating plate. Frequently corrugated fin material is placed within the ducts to aid in the absorption and transfer of heat. For aircraft use, where weight conservation is necessarily a prime objective, it is customary to construct the exchanger of light weight metals such as a aluminum alloys. Also, the plates are made thin and the fin material is formed of still thinner, ductile sheet metal. So fabricated, an exchanger is effectively reduced in weight but other problems are introduced such as the obtaining of an inexpensive, secure means of uniting the component parts of the exchanger. Also, in some uses of the exchanger high fluid pressures are encountered which may destroy too lightly a constructed device, and further, if the exchanger is in use disposed in an ambient air stream damage may result to the foil-like fins from particles entrained in the air. Extensive damage to the exchanger or at least the closing off of portions of the fluid flowing duct may result therefrom.
The instant invention has in view a concept of a light weight heat exchanger specially constructed for operation under high pressures and for resistance to air flow damage as described. Features of such concept lie in a new means of fabrication wherein the fin material serves the dual purpose of more effectively transferring heat and of acting as tie strips positively to connect adjacent plates to one another. Also, an all brazed construction is contemplated obviating the need for separable connecting devices, and, still further, a generally new fin structure is proposed characterized by the use of a relatively short length fin at the entrance end of the duct made of a heat treatable, damage resistant material and spaced from following fin material in a manner to define therewith a plenum chamber for lateral distribution of the flowing fluid.
Other objects and structural details of the invention will appear from the following description when read in connection with the accompanying drawing, wherein:
Fig. 1 is a fragmentary view of a plate type heat exchanger in accordance with the illustrated embodiment of the invention, shown in a longitudinal section taken substantially along the line 11 of Fig. 2;
Fig. 2 is a view in cross section taken substantially along the line 2-2 of Fig. 1;
Fig. 3 is a view in top longitudinal section, taken substantially along the line 33 of Fig. l; and
Fig. 4 is a view in perspective of the portion of the illustrative heat exchanger shown in Figs. 1 to 3.
Referring to the drawing, a heat exchanger in accordice ance with the illustrated embodiment of the invention comprises a series of stacked plates of a number selected in accordance with the number of fluid passes or fluid flowing ducts to be provided by the exchanger. In the example shown, four plates, 1, 2, 3 and 4 are shown. These plates have substantially the same configuration and are made of a thin light weight metal. The plates 1 and 2 are held spaced apart by marginal strips 5. Similar strips 6 hold the plates 3 and 4 in spaced relation and there is interposed between the plates 2 and 3 strip fins 7 and 8, there being further disposed between the plates 2 and 3 marginal strips 9 (one shown) as seen in Fig. 4. The fins 7 and 8 are spaced apart and define between them a plenum chamber 10.
The arrangement is one devised to bring two fluids into heat transfer relation through separating plates. To this end the marginal pieces 9 close opposite side edges of adjacent plates 2 and 3 and define therewith a fluid flowing duct open at its opposite ends for flow therethrough as indicated by the arrows in Fig. 1. The marginal pieces 5 are disposed at right angles to the pieces 9 and define with the plates 1 and 2 a duct for flow at right angles to the direction of flow in the space between plates 2 and 3. The marginal pieces 6 are arranged like the pieces 5. Thus, above and below the duct defined by plates 2 and 3, through which a first fluid flows as indicated by the arrows in Fig. l, are arranged other ducts for flow of another or other fluids in heat transfer relation tothe first fluid through respective plates 2 and 3. As indicated in Fig. 2, the upper and lower ducts as described may communicate with a common header 11 to receive a fluid flow. In the illustrated instance the header 11 and its communicating ducts constitute a part of a closed fluid flowing system, for example a lubricant circulating system. The duct for flow of the first fluid, on the other hand, is open to ambient air flow.
In the installation of the exchanger it is placed in an air duct or the like with the ram force of the moving air applied to that face of the exchanger offering open passes through the plates 2 and 3. The arrangement of the fins 7 and 8- is such as to present the longitudinal edges thereof to such air flow, the air flowing lengthwise along the fins which are corrugated to define in effect a plurality of separated longitudinal passes through the duct of the exchanger. The alternate hills and valleys of the fin are respectively in contact With the plates 2 and 3 to close off such individual passes and with the further eflect aiding in a more thorough absorption of heat from or into the flowing fluid. According to a feature of the invention the fin 7 is short in length relatively to the fin 8 and is made of a heat treatable material in order that it can be hardened and made resistant to abrasion and impact damage from particles in the flowing air stream. According to this. concept, therefore, the heat exchanger presents a hard, relatively unyielding face to the ram air there being presented only the edges of plates 1, 2, 3 and 4, the marginal pieces 5 and 6 and the edges of the fin 7. The marginal pieces 5 and 6 may also be hardened as the fin 7 so that the entire face of the exchanger is made damage resistant. The separation of the fin means 78 into two parts reduces the cost of the assembly inasmuch as the major portion of the fin means is represented by the fin 8 which may be made of the conventional untreated aluminum alloy. Also, however, such separation makes possible the plenum chamber 10 wherein a free lateral distribution of the flowing air is possible. In the presence of this chamber, therefore, a stoppage in one of the passes through the fin 7 may occur without complete loss of heat transfer ability in the longitudinal area of the exchanger in which the blocked pass lies. Should a pebble or a deformed fin portion or the like block one of the longitudinal passes through the fin 7 the air moving through the other parallel passes is free to redistribute itself in a lateral sense within the plenum chamber and to. flow through all of the passes as defined bythe fin gtincluding the one aligned with the blockedpass in The construction is one lending itself to effective fabrication. by a brazing or like process uniting the component parts securely and without likelihood of damage due to internal pressure. In the assembly of the exchanger the several parts are brought together in the manner illustrated and held in, a suitable fixture while dipped in a brazing process or otherwise unitarily connected in'a similar metal working process. Since the hills and valleys of the fin material 7 and 8 are in contact with adjacent plates these portions are united with the plate. Anueflective heat transfer connection so is made, and, in addition, a plurality of positive ties is formed between adjacent plates in a manner to resist bulging or speration of such-plates by the contained pressure of the fluids in the heat exchanger. While fin structure has been shown. only in the airflow passes it will be understood that fins may also be interposed in the closed flowing system represented by the ducts between plates 1 and 2 and between plates 3 and 4. These plates also will thus be securely tied together through the fin means. The fins are made of a thin and ductile material corrugated or crimped to the configuration shown and placed between adjacent plates of the heat exchanger with side edges of the fin strip in contact with the marginal closure pieces, the strip being in effect confined along its side edges by such marginal pieces,
What is claimed is:
1. A plate type heat exchanger constructed for weight conservation and damage resistance, including a pair of spaced apart thin metal plates of four side configuration and aligned in superposed relation to one another, closure means received between opposing side edges of said plates and defining with said platesa fluid flowing duct having opposed open entrance and exit ends, strip fin means installed in said duct including first and second strip fins made of foil-like sheet metal material of the same gauge and heat transfer capabilities and crirnped to present alternate hills and valleys in contact respectively with the opposing surfaces of said plates, one of said strip fins being relatively shorter in length than the other and made of heat treatable material and further being stationed at the entrance end of the duct ahead of the other fin, said other fin being, spaced from said one fin a distance corresponding to a substantial part of the length of said one fin to define intermediate the fins a plenum chamber for lateral distribution of fluid and said other fin extending uninterruptedly throughout the remaining length of said duct to said exit end thereof, and means uniting the assembly comprising said plates, said closures and said fins into an integrated structure.
2. A plate type heat exchanger according to claim 1, characterized by additional thin metal plates above and below said pair of plates, and closures installed in opposing side edges of adjacent plates above and below said pair of plates to. define other fluid flowing ducts in transverse relation to the first said fluid flowing duct, the last said closures being made of heat treatable material to present in conjunction with said one strip fin a damage resistant face on one side of the heat exchanger.
References Cited in the file of this patent UNITED STATES PATENTS 1,899,080 Dalgliesh Feb. 28, 1933 2,376,749 Belaieff May 22, 1945 2,566,310 Burns et al. Sept. 4, 1951 2,606,007 Simpelaar Aug. 5, 1952 2,869,835 Butt Jan. 20, 1959 enema.
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Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3322189A (en) * 1965-12-21 1967-05-30 Ford Motor Co Heat exchange assembly
US3457990A (en) * 1967-07-26 1969-07-29 Union Carbide Corp Multiple passage heat exchanger utilizing nucleate boiling
US3528496A (en) * 1967-11-03 1970-09-15 Union Carbide Corp Plate-fin heat exchanger
US3538718A (en) * 1968-12-26 1970-11-10 Phillips Petroleum Co Refrigeration evaporator heat exchanger
US3601185A (en) * 1969-11-04 1971-08-24 United Aircraft Corp Heat exchanger construction
US3880232A (en) * 1973-07-25 1975-04-29 Garrett Corp Multi-material heat exchanger construction
US3945434A (en) * 1974-09-30 1976-03-23 The Garrett Corporation Gas turbine heat exchanger apparatus
US3958631A (en) * 1972-12-11 1976-05-25 Siemens Aktiengesellschaft Heat exchanger for catalytic gas converters
US4049051A (en) * 1974-07-22 1977-09-20 The Garrett Corporation Heat exchanger with variable thermal response core
DE2733215A1 (en) * 1976-08-23 1978-03-09 Borg Warner HEAT EXCHANGER FOR CAR COMBUSTION ENGINES
FR2388238A1 (en) * 1977-04-23 1978-11-17 Sumitomo Precision Prod Co PLATE TYPE HEAT EXCHANGER
FR2479438A1 (en) * 1980-03-26 1981-10-02 Chausson Usines Sa EXCHANGER FOR COOLING A HIGH TEMPERATURE FLUID
EP0245022A1 (en) * 1986-05-01 1987-11-11 The Garrett Corporation Heat exchanger tube
US20050126769A1 (en) * 2003-12-10 2005-06-16 Honeywell International Inc. Bimetallic plate-fin titanium based heat exchanger
US20070227140A1 (en) * 2006-03-31 2007-10-04 Caterpillar Inc. Air-to-air aftercooler
US20120211215A1 (en) * 2009-11-11 2012-08-23 Kabushiki Kaisha Toyota Jidoshokki Vapor cooling heat exchanger
US20140352933A1 (en) * 2013-05-28 2014-12-04 Hamilton Sundstrand Corporation Core assembly for a heat exchanger and method of assembling
US20160025425A1 (en) * 2014-07-25 2016-01-28 Hamilton Sundstrand Corporation Heat exchanger with slotted guard fin
US20160195342A1 (en) * 2015-01-07 2016-07-07 Hamilton Sundstrand Corporation Heat exchanger with fin wave control
US10782074B2 (en) 2017-10-20 2020-09-22 Api Heat Transfer, Inc. Heat exchanger with a cooling medium bar

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1899080A (en) * 1931-10-29 1933-02-28 Res & Dev Corp Heat exchange device
US2376749A (en) * 1942-01-16 1945-05-22 Cyril Terence Delaney And Gall Radiator
US2566310A (en) * 1946-01-22 1951-09-04 Hydrocarbon Research Inc Tray type heat exchanger
US2606007A (en) * 1947-10-16 1952-08-05 Modine Mfg Co Heat exchanger
US2869835A (en) * 1957-03-11 1959-01-20 Trane Co Heat exchanger

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1899080A (en) * 1931-10-29 1933-02-28 Res & Dev Corp Heat exchange device
US2376749A (en) * 1942-01-16 1945-05-22 Cyril Terence Delaney And Gall Radiator
US2566310A (en) * 1946-01-22 1951-09-04 Hydrocarbon Research Inc Tray type heat exchanger
US2606007A (en) * 1947-10-16 1952-08-05 Modine Mfg Co Heat exchanger
US2869835A (en) * 1957-03-11 1959-01-20 Trane Co Heat exchanger

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3322189A (en) * 1965-12-21 1967-05-30 Ford Motor Co Heat exchange assembly
US3457990A (en) * 1967-07-26 1969-07-29 Union Carbide Corp Multiple passage heat exchanger utilizing nucleate boiling
US3528496A (en) * 1967-11-03 1970-09-15 Union Carbide Corp Plate-fin heat exchanger
US3538718A (en) * 1968-12-26 1970-11-10 Phillips Petroleum Co Refrigeration evaporator heat exchanger
US3601185A (en) * 1969-11-04 1971-08-24 United Aircraft Corp Heat exchanger construction
US3958631A (en) * 1972-12-11 1976-05-25 Siemens Aktiengesellschaft Heat exchanger for catalytic gas converters
US3880232A (en) * 1973-07-25 1975-04-29 Garrett Corp Multi-material heat exchanger construction
US4049051A (en) * 1974-07-22 1977-09-20 The Garrett Corporation Heat exchanger with variable thermal response core
US3945434A (en) * 1974-09-30 1976-03-23 The Garrett Corporation Gas turbine heat exchanger apparatus
DE2733215A1 (en) * 1976-08-23 1978-03-09 Borg Warner HEAT EXCHANGER FOR CAR COMBUSTION ENGINES
FR2388238A1 (en) * 1977-04-23 1978-11-17 Sumitomo Precision Prod Co PLATE TYPE HEAT EXCHANGER
FR2479438A1 (en) * 1980-03-26 1981-10-02 Chausson Usines Sa EXCHANGER FOR COOLING A HIGH TEMPERATURE FLUID
EP0245022A1 (en) * 1986-05-01 1987-11-11 The Garrett Corporation Heat exchanger tube
US20050126769A1 (en) * 2003-12-10 2005-06-16 Honeywell International Inc. Bimetallic plate-fin titanium based heat exchanger
WO2005059464A1 (en) * 2003-12-10 2005-06-30 Honeywell International Inc. Bimetallic plate-fin titanium based heat exchanger
US7201973B2 (en) 2003-12-10 2007-04-10 Honeywell International, Inc. Bimetallic plate-fin titanium based heat exchanger
US20070227140A1 (en) * 2006-03-31 2007-10-04 Caterpillar Inc. Air-to-air aftercooler
US7878233B2 (en) * 2006-03-31 2011-02-01 Caterpillar Inc Air-to-air aftercooler
US20120211215A1 (en) * 2009-11-11 2012-08-23 Kabushiki Kaisha Toyota Jidoshokki Vapor cooling heat exchanger
US20140352933A1 (en) * 2013-05-28 2014-12-04 Hamilton Sundstrand Corporation Core assembly for a heat exchanger and method of assembling
US20160025425A1 (en) * 2014-07-25 2016-01-28 Hamilton Sundstrand Corporation Heat exchanger with slotted guard fin
US20160195342A1 (en) * 2015-01-07 2016-07-07 Hamilton Sundstrand Corporation Heat exchanger with fin wave control
US10782074B2 (en) 2017-10-20 2020-09-22 Api Heat Transfer, Inc. Heat exchanger with a cooling medium bar

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