[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

US3775972A - Heat exchanger mounting - Google Patents

Heat exchanger mounting Download PDF

Info

Publication number
US3775972A
US3775972A US00222125A US3775972DA US3775972A US 3775972 A US3775972 A US 3775972A US 00222125 A US00222125 A US 00222125A US 3775972D A US3775972D A US 3775972DA US 3775972 A US3775972 A US 3775972A
Authority
US
United States
Prior art keywords
heat exchanger
face
exchanger core
high pressure
inlet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US00222125A
Other languages
English (en)
Inventor
R Perpall
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Garrett Corp
Original Assignee
Garrett Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Garrett Corp filed Critical Garrett Corp
Application granted granted Critical
Publication of US3775972A publication Critical patent/US3775972A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/0219—Arrangements for sealing end plates into casing or header box; Header box sub-elements
    • F28F9/0224—Header boxes formed by sealing end plates into covers
    • F28F9/0226—Header boxes formed by sealing end plates into covers with resilient gaskets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04—Cooling of air intake supply
    • F02B29/045—Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly
    • F02B29/0456—Air cooled heat exchangers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Definitions

  • ABSTRACT Resilient elements are provided for the mounting of a heat exchanger core between structurally joined inlet and outlet ducts.
  • the present invention provides a heat exchanger particularly adaptable for use in generally adverse environments.
  • Theheat exchanger core is provided with a gasket or sealing element of a resilient or elastomeric material on both the inlet face and outlet face thereof.
  • This gasket may extend a short distance around the side of the heat exchanger core away from the inlet and outlet faces thereof respectively;
  • the heat exchanger core does not include any flanges or other structurally supporting mounting means.
  • the inlet duct and outlet duct on opposite sides of the heat exchanger are structurally connected to compress the gasket both on the inlet and outlet faces of the heat exchangercore and along the side edges of the inlet and outlet faces thereof.
  • FIG. 1 is a frontal elevation of the heat exchanger core of the present invention
  • FIG. 2 is a side elevation of the heat exchanger core of the present invention
  • FIGS. 1, 2 and 3 illustrate a conventional, cross flow, plate-fin heat exchanger including offset corrugated tins in the separate fluid passageways.
  • the frontal view shown. in FIG. 1 illustrates the inletface 11 of the high pressure side or hot fluid side of the heat exchanger core 10.
  • the hot fluid or high pressure passages 12 separated by header bars 14 to prevent hot fluid flow into the cold fluid passages are also shown.
  • the resilient material or elastomeric gasket 16 is shown extending around the entire periphery of the inlet face 11 of the heat exchanger core 10. As more clearly shown in FIGS. 2 and 3, the gasket 16 in- "cludes a side extension or wrap around portion 18 which extends around two opposed edges of the heat exchanger inlet face 11.
  • the side view of the heat exchanger core 10 illustrated in FIG. 2 shows the low pressure inlet face which includes cold fluid passageways 20 and side header bars 22.
  • the top view, FIG. 3, is partially cut away to show a cold fluid passage 20 and hot fluid passage 12,
  • the configuration of the gasket 16 is more clearly illustrated in FIGS. .4, 5 and 6.
  • the gasket includes a first flat face 30 which abuts the inlet face 11 of the heat exchanger core and a second flat face 32 disposed at a angle to the first flat face 30 to extend along the side face 19 of the heat exchanger core 10 adjacent to the inlet face 11.
  • the main portion of the gasket, which extends around the entire inlet face 11, includes an outwardprojection 34 having a substantially flat outer surface disposed at a slight angle from the plane of the inlet face 11.
  • the inlet duct associated with the heat exchanger core 10 will include a flange 40 having a flat face in substantially the same plane as the inlet face 11. of the heat exchanger core 10 so as to compress the gasket projection 34 towards the same plane as the inlet face 11.
  • the inletduct would also include a flange 42 to compress the side extending or wrap around portion 18 of the gasket 16 along the face 19 of the heat exchanger core 10. This flange 42 should be slightly flared to facilitate positioning of the core 10 and compression of the gasket.
  • the heat exchanger mounting of the present invention is particularly adapted for use in adverse environments such as on a vehicular engine.
  • the heat exchanger core 10 including a gasket 16 on both the hot fluid inlet and outlet faces thereof, is disposed between a compressed air duct 50 which receives compressed air from an engine turbocharger compressor 52, and the engine inlet manifold 54 which includes a manifold duct 56.
  • the compressed air duct 50 and inlet manifold duct 56 includes flanges 58 and 60 respectively to engage the gaskets 16 on the heat exchanger core 10.
  • a plurality of tie rods 62 together with structural sections of the inlet manifold duct 56, are used to join the compressed air duct 50 and inlet manifold duct 56 to secure the heat exchanger core 10 therebetween. Cooled air may be passed through the low pressure or cold side of the heat exchanger core 10 by a tip-turbine driven fan 64 which is driven by a portion of the compressed air from the turbocharger compressor 52 through bypass duct 66.
  • the gasket 16 may be of any resilient material such as a silicone elastomer (Silastic, a trademark of Dow Coming).
  • the gasket material must be selected to provide reasonable life when subjected to the operating environment in which the heat exchanger is to be used.
  • the gasket in most instances would be bonded to the inlet and outlet faces in the heat exchanger core by a Room Temperature vulcanizing (RTV) Silicone Elastomer.
  • RTV Room Temperature vulcanizing
  • the core can then be inserted directly into the cavity in the ducts carrying the fluid to be cooled and the assembly squeezed to a predetermined dimension by means of the tie bolts or other flange joining means.
  • the heat exchanger core does not require any integral flanges or machining operations prior to its use.
  • the ducts in which the heat exchanger core is to be inserted can be of cast material and likewise do not require any machining operations before use.
  • the side extending positions of the gaskets provide considerable resistance to vibration in all directions. This wrap around feature is exceedingly important in the vehicular applications. In order to insure that the resonant vibration frequency of the heat exchanger core is always higher than any driving frequency present, the squeeze or pressure on the gasket should be controlled.
  • Heat exchangers mounted in accordance with the present invention provide adequate sealing for the high pressure or hot fluid, while effectively preventing vibratory, thermal expansion or rigging stress from being transmitted to the fragile heat exchanger core.
  • the mounting costs are reduced since no machining operations are required.
  • the heat exchanger core can be easily replaced or removed for cleaning without damaging or replacing the more costly ducts.
  • a heat exchanger core having a high pressure inlet face and a high pressure outlet face
  • an inlet duct disposed to provide high pressure fluid to the high pressure inlet face of said heat exchanger core
  • said duct joining means at least partially compressing the first resilient gasket between the inlet duct and the high pressure inlet face of said heat exchanger core and at least partially compressing the second resilient gasket between the outlet duct and the high pressure outlet face of said heat exchanger core.
  • said duct joining means includes a plurality of tie rods extending between said inlet duct and said outlet duct.
  • cooling air driving means operably associated with said heat exchanger core, said cooling air driving means driven by compressed air from the turbocharger compressor.
  • cooling air driving means is a tip turbine driven fan.
  • a heat exchanger core having a high pressure inlet face and a high pressure outlet face
  • first resilient gasket disposed around the periphery of the high pressure inlet face of said heat exchanger core, said first resilient gasket having an inner substantially flat face in contact with the inlet face of said heat exchanger core and an outer substantially flat face generally opposed to said inner flat face and projecting slightly outward therefrom;
  • a second resilient gasket disposed around the periphery of the high pressure outlet face of said heat exchanger core, said second resilient gasket having an inner substantially flat face in contact with the outlet face of said heat exchanger core and an outer substantially flat face generally opposed to said inner flat face and projecting slightly outward therefrom;
  • an inlet duct disposed to provide high pressure fluid to the high pressure inlet face of said heat exchanger core
  • said duct joining means at least partially compressing the projecting outer face of the first resilient gasket towards the inner face thereof between the inlet duct and the high pressure inlet face of said heat exchanger core and at least partially compressing the projecting outer face of the second resilient gasket toward the inner face thereof between the outlet duct and the high pressure outlet face of said heat exchanger core.
  • said duct joining means includes a plurality of tie rods extending between said ducts.
  • a heat exchanger core having a high pressure inlet face, an opposedhigh pressure outlet face, and two low pressure faces extending therebetween;
  • first resilient gasket disposed around the periphery of the high pressure inlet face of said. heat exchanger core, said first resilient gasket having a first inner substantially flat face in contact with the inlet face of said heat exchanger core, an outer substantially flat face generally opposed to said inner flatface and projecting slightly outward therefrom, and a second substantially flat inner face in contact with at least a portion of the edge of the low pres sure faces adjacent said inlet face;
  • a second resilient gasket disposed around the periphery of the high pressure outlet face of said heat exchanger core, said second resilient gasket having a first inner substantially flat face in contact with the outlet face of said heat exchanger core, an outer substantially flat face generally opposed to said r inner flat face and projecting slightly outward therefrom, and a second substantially flat inner face in contact with at least a portion of the edge of the low pressure faces adjacent said outlet face;
  • an inlet duct disposed to receive the high pressure inlet face of said heat exchanger core and to provide high pressure fluid thereto;
  • said duct joining means at least partially compressing the first resilient gasket between the inlet duct and the high pressure inlet face and adjacent side faces of said heat exchanger core and at least partially compressing the second resilient gasket between the outlet duct and the high pressure outlet face and adjacent side faces of said heat exchanger core.
  • a heat exchanger core having a high pressure inlet face, an opposed high pressure outlet face, and two low pressure faces extending therebetween;
  • first resilient gasket disposed around the periphery of the high pressure inlet face of said heat exchanger core, said first resilient gasket having a first inner substantiallyflat face in contact with the inlet face of said heat exchanger core, an outer substantially flat face generally opposed to said inner flat face and projecting slightly outward therefrom, and a second substantially flat inner face in contact with at least a portion of the edge of the low pressure faces adjacent said inlet face;
  • a second resilient gasket disposed around the periphery of the high pressure outlet face of said heat exchanger core, said second resilient gasket having a first inner substantially flat face in contact with the ,outlet face of said heat exchanger core, an outer substantially flat face generally opposed to said inner flat face and projecting slightly outward therefrom, and a second substantially flat inner face in contact with at leasta portion of the edge of the low pressure faces adjacent said outlet face;
  • an inlet duct disposed to provide high pressure fluid to the high pressure inlet face of said heat exchanger, said inletduct having a heat exchanger core inlet face receiving flange;
  • outlet duct disposed to receive high pressure fluid from the high pressure outlet. faceof said heat exchanger, said outlet duct having a heat exchanger core outlet face receiving flange, and
  • said duct joining means at least partially compressing thefirst resilient gasket between i the inlet duct and the high pressure inlet face and adjacent side faces of said heat exchanger core and at least partially compressing the second resilient gasket between the outlet duct and the high pressure outlet face and adjacent side faces of said heat exchanger core.
  • a heat exchanger core having a high pressure inlet face and a high pressure outlet face
  • an engine to propel a vehicle said engine producing exhaust gases and having an intake manifold to receive compressed combustion air;
  • a turbocharger mounted on said engine to receive exhaust gases therefrom and produce compressed combustion air for said engine
  • turbocharger having a compressed air duct to provide compressed air to the high pressure inlet face of said heat exchanger core
  • said inlet manifold having a duct to receive compressedair from the high pressure outlet face of said heat exchanger core
  • said duct joining means at least parand second resilient gaskets are of a silicone elastomer.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
US00222125A 1972-01-31 1972-01-31 Heat exchanger mounting Expired - Lifetime US3775972A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US22212572A 1972-01-31 1972-01-31

Publications (1)

Publication Number Publication Date
US3775972A true US3775972A (en) 1973-12-04

Family

ID=22830944

Family Applications (1)

Application Number Title Priority Date Filing Date
US00222125A Expired - Lifetime US3775972A (en) 1972-01-31 1972-01-31 Heat exchanger mounting

Country Status (6)

Country Link
US (1) US3775972A (de)
JP (1) JPS4884341A (de)
DE (1) DE2302855C2 (de)
FR (1) FR2173976B1 (de)
GB (1) GB1418767A (de)
IT (1) IT977145B (de)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4023618A (en) * 1975-08-18 1977-05-17 Union Carbide Corporation Heat exchanger headering arrangement
US4262740A (en) * 1979-02-07 1981-04-21 Heinz Brune Casings for heat exchangers and burner/recuperator assemblies incorporating such casings
US4303052A (en) * 1980-03-24 1981-12-01 The Garrett Corporation Charge air cooler mounting arrangement
US4333522A (en) * 1979-02-07 1982-06-08 Heinz Brune Casings for heat exchangers and burner/recuperator assemblies incorporating such casings
US4596285A (en) * 1985-03-28 1986-06-24 North Atlantic Technologies, Inc. Heat exchanger with resilient corner seals
US4722387A (en) * 1986-02-18 1988-02-02 The Garrett Corporation Heat exchanger and method of assembly
US4916902A (en) * 1986-02-14 1990-04-17 Pratt Howard L Ambient air modulator for engine fluid heat exchanger
US20050082044A1 (en) * 2000-10-31 2005-04-21 Haruo Miura Heat exchanger for air compressor
US6971438B2 (en) * 2000-12-28 2005-12-06 Honda Giken Kogyo Kabushiki Kaisha Vehicle radiator device
US20060266506A1 (en) * 2005-05-27 2006-11-30 Lg Electronics Inc. Heat exchanger for dryer and condensing type dryer using the same
US20120134653A1 (en) * 2009-06-23 2012-05-31 Cinier Radiateurs, Sarl Reversible radiator
US20120132396A1 (en) * 2010-11-29 2012-05-31 Denso Corporation Air conditioning system for vehicle
WO2013135546A1 (de) * 2012-03-15 2013-09-19 Mahle International Gmbh Ladeluftkühleinrichtung
US20140116664A1 (en) * 2012-10-31 2014-05-01 The Boeing Company Cross-Flow Heat Exchanger Having Graduated Fin Density
WO2015137871A1 (en) * 2014-03-12 2015-09-17 Scania Cv Ab Arrangement for fastening of a radiator in an air duct

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2476297A1 (fr) * 1980-02-19 1981-08-21 Ferodo Sa Dispositif d'etancheite, en particulier pour le montage d'un echangeur de chaleur dans une installation de chauffage et/ou de climatisation, notamment d'un vehicule automobile
US4823868A (en) * 1988-05-26 1989-04-25 Deere & Company Intercooler and method of assembling the same
US6269996B1 (en) 1999-08-06 2001-08-07 Robbins, Inc. Fastener driving apparatus and method

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US223835A (en) * 1880-01-27 Pipe-coupling
US1840417A (en) * 1930-03-19 1932-01-12 Mcquay Radiator Corp Frame and mounting for heat exchange units
US2004151A (en) * 1932-12-27 1935-06-11 E A Lab Inc Heater apparatus
US2340853A (en) * 1941-06-27 1944-02-08 Fred M Young Heat exchanger for superchargers
US2512748A (en) * 1945-02-12 1950-06-27 Worthington Pump & Mach Corp Expansion joint for heat exchangers
GB877353A (en) * 1959-03-31 1961-09-13 Serck Radiators Ltd Improvements in mountings for air-cooled radiators
US3610324A (en) * 1969-10-15 1971-10-05 Hudson Products Corp Air cooler apparatus

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE304850C (de) *
CH44279A (fr) * 1908-03-09 1909-07-16 Anonima Per Frigorigeni E Moto Appareil pour l'échange de chaleur entre des fluides sous pression
CH114976A (fr) * 1925-07-07 1926-05-17 Mario Lava Radiateur démontable pour moteurs à explosion.
US2342164A (en) * 1941-08-30 1944-02-22 Pinkel Benjamin Heat exchanger
DE742695C (de) * 1942-03-28 1953-05-26 Daimler Benz Ag Profilabdichtung, insbesondere fuer Blechhauben von Brennkraftmaschinen
DE1079892B (de) * 1956-06-11 1960-04-14 Inst Schienenfahrzeuge Kuehler mit auswechselbaren Kuehlerteilbloecken
US3415315A (en) * 1966-06-29 1968-12-10 Borg Warner Heat exchanger

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US223835A (en) * 1880-01-27 Pipe-coupling
US1840417A (en) * 1930-03-19 1932-01-12 Mcquay Radiator Corp Frame and mounting for heat exchange units
US2004151A (en) * 1932-12-27 1935-06-11 E A Lab Inc Heater apparatus
US2340853A (en) * 1941-06-27 1944-02-08 Fred M Young Heat exchanger for superchargers
US2512748A (en) * 1945-02-12 1950-06-27 Worthington Pump & Mach Corp Expansion joint for heat exchangers
GB877353A (en) * 1959-03-31 1961-09-13 Serck Radiators Ltd Improvements in mountings for air-cooled radiators
US3610324A (en) * 1969-10-15 1971-10-05 Hudson Products Corp Air cooler apparatus

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4023618A (en) * 1975-08-18 1977-05-17 Union Carbide Corporation Heat exchanger headering arrangement
US4262740A (en) * 1979-02-07 1981-04-21 Heinz Brune Casings for heat exchangers and burner/recuperator assemblies incorporating such casings
US4333522A (en) * 1979-02-07 1982-06-08 Heinz Brune Casings for heat exchangers and burner/recuperator assemblies incorporating such casings
US4303052A (en) * 1980-03-24 1981-12-01 The Garrett Corporation Charge air cooler mounting arrangement
US4596285A (en) * 1985-03-28 1986-06-24 North Atlantic Technologies, Inc. Heat exchanger with resilient corner seals
US4916902A (en) * 1986-02-14 1990-04-17 Pratt Howard L Ambient air modulator for engine fluid heat exchanger
US4722387A (en) * 1986-02-18 1988-02-02 The Garrett Corporation Heat exchanger and method of assembly
US7172015B2 (en) * 2000-10-31 2007-02-06 Hitachi Plant Technologies, Ltd. Heat exchanger for air compressor
US20050082044A1 (en) * 2000-10-31 2005-04-21 Haruo Miura Heat exchanger for air compressor
US6971438B2 (en) * 2000-12-28 2005-12-06 Honda Giken Kogyo Kabushiki Kaisha Vehicle radiator device
US20060266506A1 (en) * 2005-05-27 2006-11-30 Lg Electronics Inc. Heat exchanger for dryer and condensing type dryer using the same
US20120134653A1 (en) * 2009-06-23 2012-05-31 Cinier Radiateurs, Sarl Reversible radiator
US9234666B2 (en) * 2009-06-23 2016-01-12 Michel Cinier Heat transfer apparatus for heating and cooling a room
US20120132396A1 (en) * 2010-11-29 2012-05-31 Denso Corporation Air conditioning system for vehicle
US9267738B2 (en) * 2010-11-29 2016-02-23 Denso Corporation Rigid and elastic mounting for vehicle heat exchanger
WO2013135546A1 (de) * 2012-03-15 2013-09-19 Mahle International Gmbh Ladeluftkühleinrichtung
US9951677B2 (en) 2012-03-15 2018-04-24 Mahle International Gmbh Charge-air cooling device
US20140116664A1 (en) * 2012-10-31 2014-05-01 The Boeing Company Cross-Flow Heat Exchanger Having Graduated Fin Density
US9377250B2 (en) * 2012-10-31 2016-06-28 The Boeing Company Cross-flow heat exchanger having graduated fin density
WO2015137871A1 (en) * 2014-03-12 2015-09-17 Scania Cv Ab Arrangement for fastening of a radiator in an air duct

Also Published As

Publication number Publication date
IT977145B (it) 1974-09-10
FR2173976A1 (de) 1973-10-12
DE2302855A1 (de) 1973-08-09
GB1418767A (en) 1975-12-24
DE2302855C2 (de) 1983-03-10
FR2173976B1 (de) 1976-05-14
JPS4884341A (de) 1973-11-09

Similar Documents

Publication Publication Date Title
US3775972A (en) Heat exchanger mounting
US3858291A (en) Method of mounting a heat exchanger core
KR960012125B1 (ko) 중간 냉각기 및 그 조립 방법
CN105909370A (zh) 用于使用液体冷却剂冷却压缩空气流的热交换器
US5577900A (en) Turbocharged internal combustion engine
US10605545B2 (en) Heat exchanger and core for a heat exchanger
JP6383801B2 (ja) 自動車両用の熱交換器
US6805108B2 (en) Heat exchanger for a supercharger
US20170108283A1 (en) Heat exchanger for a motor vehicle
US3741293A (en) Plate type heat exchanger
JP2001248448A (ja) 内燃機関の給気冷却装置
JPS62293086A (ja) 積層型熱交換器
US5697217A (en) Turbocharged internal combustion engine
JP2013092181A (ja) ガスケット
EP0680552B1 (de) Vorrichtung zur befestigung und abdichtung eines einlassluftzwischenkühlers
US20060096286A1 (en) Charge air cooler
US20100059010A1 (en) Heat Insulator For An Intake Manifold Of An Air-Cooled Charge Air Cooler
GB2617633A (en) Integral cooling system for turbine casing and guide vanes in aeroengine
JP5671907B2 (ja) Ｅｇｒガス冷却装置
JPS5979011A (ja) 蒸気タ−ビンのボルトク−リング法
CA1169851A (en) Heat exchanger core resilient support and seal
CN215444167U (zh) 一种涡轮发电机组内部散热结构
JP3453928B2 (ja) 内燃機関のインタクーラ
JPH05322475A (ja) 装入空気冷却器及びその製造方法
JPH0435608B2 (de)