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US3034770A - Heat exchanger - Google Patents

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Publication number
US3034770A
US3034770A US840379A US84037959A US3034770A US 3034770 A US3034770 A US 3034770A US 840379 A US840379 A US 840379A US 84037959 A US84037959 A US 84037959A US 3034770 A US3034770 A US 3034770A
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United States
Prior art keywords
passages
heat exchanger
tank
header
core
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Expired - Lifetime
Application number
US840379A
Inventor
Frederick A Hiersch
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Continental Aviation and Engineering Corp
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Continental Aviation and Engineering Corp
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Publication date
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Priority to US840379A priority Critical patent/US3034770A/en
Application granted granted Critical
Publication of US3034770A publication Critical patent/US3034770A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F28D1/00Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • F28D1/02Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
    • F28D1/0246Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid heat-exchange elements having several adjacent conduits forming a whole, e.g. blocks
    • 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
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0049Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for lubricants, e.g. oil coolers

Definitions

  • My invention relates to heat exchangers and more particularly to heat exchangers of the type having a core provided with passages for one fluid being disposed normal to the passages for another fluid, such as is used in heat exchangers commonly called radiators.
  • heat exchangers generally involves tedious and expensive hand assembly and welding operations, and quality control is very diilicult to achieve.
  • heat exchangers are quite pronel to leakage and blowout, particularly where one of the fluids is under pressure and/ or subject to pressure pulsing which readily produces structural failure and blowout even when static pressure tests have been passed satisfactorily.
  • An object of the present invention is to decrease failure of heat exchangers by providing an improved construction having overall reinforcements against blowout from normal operation and from excessive ⁇ iiuid pressure.
  • Another object of the invention is to facilitate quality control by providing a heat exchanger structure adaptable to automatic assembly and welding operations.
  • a further object of the invention is to improve heat exchanger construction by providing fluid warmup and bypass return tubes which are the full width of the core plates and in combination with a tank and header provide overall reinforcement for the core.
  • FIG. l is a side elevational view of a heat exchanger constructed in accordance with the present invention.
  • FIG. 2 is an end elevational view of the tank structure side of the heat exchanger of FIG. l.
  • FIG. 3 is a top view of the heat exchanger of FIG. l.
  • FIG. 4 is a cross sectional view of the tank structure taken substantially on the line 4 4 of FIG. 2.
  • FIG. 5 is a fragmentary cross-sectional view taken substantially on the line 5 5 of FIG. l.
  • FIG. 6 is a flow diagram of the heat exchanger.
  • the heat exchanger is illustrated as comprising a tank structure 1li, a header structure 11, and a core structure 12 sandwiched between the tank and header structures 1t) and 11.
  • the tank structure comprises a housing 13 having an inlet passage 15, an outlet port 16 opening to an outlet chamber 17 as shown in FIG. l, and a bypass passage 18 connected with the outlet chamber and controlled by a thermostatic bypass valve 19 as illustrated in FIG. 4.
  • the header structure comprises a housing 20 having a manifold chamber- 21.
  • the core structure comprises a pair of substantially similar parallel rigid Wall structures 25 and 26 connecting opposite sides of the tank structure 10 with opposite sides of the header structure 11 preferably by brazing or welding to form a rigid substantially parallelepipedshaped casing 1li.
  • Each wall structure preferably comprises an outer member 27 having ribs 2S as shown in FIG. 5, and an inner flat plate 29 abutting the ribs 23 to form a plurality of longitudinal inlet warm-up passages 30 in the wall structure 25 and a plurality of bypass passages 31 in the wall structure 26. If desired,
  • the warm up passages 30 openly connect the tank inlet passage 1'5 with the header manifold chamber 21.
  • the bypass passages 31 openly connect the header manifold chamber 21 with the tank bypass passage 18.
  • Each of the core elements 32 has a plurality of longitudinal passages 35 openly connecting the tank outlet chamber 17 with the header manifold chamber 21.
  • Each of the core elements 33 is corrugated as shown to provide a plurality of lateral passages 36 disposed normal to the passages 35 and open from opposite sides of the core structure 12.
  • Substantially rigid longitudinal bar elements 40 are secured along the sides of each core element 32 parallel with the passages 35, and substantially rigid lateral bar elements 41 are secured along the sides of each core element 33 parallel with the passages 36.
  • the various components of the heat exchanger are preferably welded or brazed together, and it will be seen that the wall structures 25 and 26 having passages 30 and 31 and the tank and header structures 10 and 11,
  • the intake and outlet ports 14 and 16 are preferably adapted for connection to an oil or other fluid system (not shown) under pressure.
  • the core element passages 36 are preferably adapted to conduct cooling air iiow.
  • the oil or other fluid entering the port 14 passes through the intake passage 1'5 and the warmup passages 3l) to the header manifold chamber 21.
  • the thermostatic valve 19 is adapted to open the bypass passage 18 to the outlet chamber 17, so that the passages 31 will pass at least part of the oil flow from the header manifold chamber 21 direct to the tank outlet chamber 17.
  • the thermostatic valve 19 is adapted to close the bypass passage 18, so that oil iiow passes from the header manifold chamber 21 through the passages 32, in heat exchange relation with the cooling air passages 36, to the tank outlet chamber 17.
  • a uid to fluid heat exchanger comprising a tank structure having an inlet passage and an outlet chamber, a header structure spaced from the tank structure and having a manifold compartment, and a core structure sandwiched intermediate said tank structure and said header structure, said core structure comprising a pair of spaced rigid parallel walls connecting opposite sides of said tank structure with opposite sides of said header structure, said header structure, tank structure and connecting walls forming a substantially parallelepiped-shaped casing assembly, said walls each extending the full width of said tank structure and said header structure, one of said walls having at least one longitudinal warm-up passage openly connecting said tank inlet passage with said header manifold compartment, a plurality of parallel stacked core elements sandwiched intermediate and parallel with said Walls, alternate core elements having 1ongitudinal passages openly connecting said header manifold compartment with said tank outlet chamber, the

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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 15, 1962 F. A. Hll-:Rscl-l HEAT EXCHANGER 2 Sheets-Sheet l Filed Sept. 16, 1959 IN V EN TOR.
I I I I l FREDERICK A.HI ER SCH BY F. A. HIERSCH HEAT EXCHANGER May 15, 1962 2 Sheets-Sheet 2 Filed Sept. 16, 1959 mm Nm Ov mN mw NN INVENTOR.
FREDERICK A.||||-:RscH
ATTORNE s United States Patent O 3,034,770 HEAT EXCGER Frederick A. Hiersch, Detroit, Mich., assior to Continental Aviation and Engineering Corporation, Detroit, Mich., a corporation of Virginia Filed Sept. 16, 1959, Ser. No. 840,379 4 Claims. (Cl. 257-245) My invention relates to heat exchangers and more particularly to heat exchangers of the type having a core provided with passages for one fluid being disposed normal to the passages for another fluid, such as is used in heat exchangers commonly called radiators.
The manufacture of such heat exchangers generally involves tedious and expensive hand assembly and welding operations, and quality control is very diilicult to achieve. Moreover, such heat exchangers are quite pronel to leakage and blowout, particularly where one of the fluids is under pressure and/ or subject to pressure pulsing which readily produces structural failure and blowout even when static pressure tests have been passed satisfactorily.
An object of the present invention is to decrease failure of heat exchangers by providing an improved construction having overall reinforcements against blowout from normal operation and from excessive `iiuid pressure.
Another object of the invention is to facilitate quality control by providing a heat exchanger structure adaptable to automatic assembly and welding operations.
A further object of the invention is to improve heat exchanger construction by providing fluid warmup and bypass return tubes which are the full width of the core plates and in combination with a tank and header provide overall reinforcement for the core.
For a more complete understanding of the invention, reference may be had to the accompanying drawings illustrating a preferred embodiment of the invention in which like reference characters refer to like parts throughout the several views and in which FIG. l is a side elevational view of a heat exchanger constructed in accordance with the present invention.
FIG. 2 is an end elevational view of the tank structure side of the heat exchanger of FIG. l.
FIG. 3 is a top view of the heat exchanger of FIG. l.
FIG. 4 is a cross sectional view of the tank structure taken substantially on the line 4 4 of FIG. 2.
FIG. 5 is a fragmentary cross-sectional view taken substantially on the line 5 5 of FIG. l, and
FIG. 6 is a flow diagram of the heat exchanger.
The heat exchanger is illustrated as comprising a tank structure 1li, a header structure 11, and a core structure 12 sandwiched between the tank and header structures 1t) and 11.
The tank structure comprises a housing 13 having an inlet passage 15, an outlet port 16 opening to an outlet chamber 17 as shown in FIG. l, and a bypass passage 18 connected with the outlet chamber and controlled by a thermostatic bypass valve 19 as illustrated in FIG. 4.
The header structure comprises a housing 20 having a manifold chamber- 21.
The core structure comprises a pair of substantially similar parallel rigid Wall structures 25 and 26 connecting opposite sides of the tank structure 10 with opposite sides of the header structure 11 preferably by brazing or welding to form a rigid substantially parallelepipedshaped casing 1li. Each wall structure preferably comprises an outer member 27 having ribs 2S as shown in FIG. 5, and an inner flat plate 29 abutting the ribs 23 to form a plurality of longitudinal inlet warm-up passages 30 in the wall structure 25 and a plurality of bypass passages 31 in the wall structure 26. If desired,
ice
the outer member 27, ribs 28 and plate 29 could be formed as a single piece extrusion. The warm up passages 30 openly connect the tank inlet passage 1'5 with the header manifold chamber 21. The bypass passages 31 openly connect the header manifold chamber 21 with the tank bypass passage 18.
Sandwiched between the wall structures 25 and 26 in the casing 10A, or more particularly between the plates 28, are parallel alternately stacked core elements 32 and 33 separated by flat plates 34. Each of the core elements 32 has a plurality of longitudinal passages 35 openly connecting the tank outlet chamber 17 with the header manifold chamber 21. Each of the core elements 33 is corrugated as shown to provide a plurality of lateral passages 36 disposed normal to the passages 35 and open from opposite sides of the core structure 12.
Substantially rigid longitudinal bar elements 40 are secured along the sides of each core element 32 parallel with the passages 35, and substantially rigid lateral bar elements 41 are secured along the sides of each core element 33 parallel with the passages 36.
The various components of the heat exchanger are preferably welded or brazed together, and it will be seen that the wall structures 25 and 26 having passages 30 and 31 and the tank and header structures 10 and 11,
form a full width casing which provides overall reinforcement and effectively contain the core elements 32 and 33 against blow out from excessive or pulsating pressures.
The intake and outlet ports 14 and 16 are preferably adapted for connection to an oil or other fluid system (not shown) under pressure. The core element passages 36 are preferably adapted to conduct cooling air iiow. The oil or other fluid entering the port 14 passes through the intake passage 1'5 and the warmup passages 3l) to the header manifold chamber 21. When the oil is cold, the thermostatic valve 19 is adapted to open the bypass passage 18 to the outlet chamber 17, so that the passages 31 will pass at least part of the oil flow from the header manifold chamber 21 direct to the tank outlet chamber 17. When the oil is warm, the thermostatic valve 19 is adapted to close the bypass passage 18, so that oil iiow passes from the header manifold chamber 21 through the passages 32, in heat exchange relation with the cooling air passages 36, to the tank outlet chamber 17.
Although I have described only one preferred embodiment of my invention, it will be apparent to one skilled in the art to which the invention pertains that various changes and modifications may be made therein without departing from the spirit of the invention or the scope of the appended claims.
I claim:
1. A uid to fluid heat exchanger comprising a tank structure having an inlet passage and an outlet chamber, a header structure spaced from the tank structure and having a manifold compartment, and a core structure sandwiched intermediate said tank structure and said header structure, said core structure comprising a pair of spaced rigid parallel walls connecting opposite sides of said tank structure with opposite sides of said header structure, said header structure, tank structure and connecting walls forming a substantially parallelepiped-shaped casing assembly, said walls each extending the full width of said tank structure and said header structure, one of said walls having at least one longitudinal warm-up passage openly connecting said tank inlet passage with said header manifold compartment, a plurality of parallel stacked core elements sandwiched intermediate and parallel with said Walls, alternate core elements having 1ongitudinal passages openly connecting said header manifold compartment with said tank outlet chamber, the
other core elements having lateral passages disposed substantially normal to the first core element passages and opening at opposite sides of said heat exchanger.
2. The heat exchanger as defined in claim 1 and in which said tank structure has a bypass passage communicating with said outlet chamber, a valve in said bypass passage, and the other of said walls having at least one longitudinal passage openly connecting said header manifold compartment with said bypass passage.
3. The heat exchanger as dened in claim 2 and in which said Walls each comprise an outer plate member having a plurality of spaced longitudinal ribs forming parallel channels and an inner flat plate member covering said ribs and channels.
4. The heat exchanger as defined in claim l and in which at plates separate adjacent core elements and in which a substantially rigid bar element is secured along each side of each core element and extends parallel to the passages therein, said bar elements being sandwiched between and spacing apart the edges of said at plates.
References Cited in the file of this patent UNITED STATES PATENTS 2,360,123 Gerstung et al. Oct. 10, 1944
US840379A 1959-09-16 1959-09-16 Heat exchanger Expired - Lifetime US3034770A (en)

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3450197A (en) * 1965-02-06 1969-06-17 Ferodo Sa Heat exchangers
US3800861A (en) * 1969-12-05 1974-04-02 Gen Electric Air cooled vapor condenser module
US5555930A (en) * 1994-06-24 1996-09-17 Behr Heat Transfer, Inc. Heat exchanger assembly with structural side passageways
BE1009342A3 (en) * 1993-11-18 1997-02-04 Henco Ind Naamloze Vennootscha HEATING ELEMENT.
US5950715A (en) * 1995-06-16 1999-09-14 Alfa Laval Ab Plate heat exchanger
US6527046B1 (en) * 1999-06-02 2003-03-04 Akg Of America, Inc. Heat exchanger, particularly oil cooler
WO2004005832A1 (en) * 2002-07-04 2004-01-15 Hydac S.A. Device for heat exchange between flowable media
US20040112577A1 (en) * 2002-09-12 2004-06-17 Ralf Beck Radiator with side flat tubes
US6779591B2 (en) * 2000-08-25 2004-08-24 Modine Manufacturing Company Compact heat exchanger for a compact cooling system
US20050126517A1 (en) * 2003-12-12 2005-06-16 Visteon Global Technologies, Inc. Integrated heat exchange and fluid control device
US20060076129A1 (en) * 2004-10-13 2006-04-13 Visteon Global Technologies, Inc. Integrated thermal bypass valve
US20070175612A1 (en) * 2003-10-02 2007-08-02 Behr Gmbh & Co. Kg Charge intercooler for a motor vehicle
US20120125594A1 (en) * 2010-11-18 2012-05-24 Hamilton Sundstrand Corporation Heat Exchanger System
DE102014010632A1 (en) 2014-07-17 2016-01-21 Modine Manufacturing Company Soldered heat exchanger and manufacturing process
FR3060057A1 (en) * 2016-12-14 2018-06-15 Safran Aircraft Engines FLUIDIC CIRCUIT IN A TURBOMACHINE

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2360123A (en) * 1942-09-18 1944-10-10 Gen Motors Corp Oil cooler

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2360123A (en) * 1942-09-18 1944-10-10 Gen Motors Corp Oil cooler

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3450197A (en) * 1965-02-06 1969-06-17 Ferodo Sa Heat exchangers
US3800861A (en) * 1969-12-05 1974-04-02 Gen Electric Air cooled vapor condenser module
BE1009342A3 (en) * 1993-11-18 1997-02-04 Henco Ind Naamloze Vennootscha HEATING ELEMENT.
US5555930A (en) * 1994-06-24 1996-09-17 Behr Heat Transfer, Inc. Heat exchanger assembly with structural side passageways
US5950715A (en) * 1995-06-16 1999-09-14 Alfa Laval Ab Plate heat exchanger
US6527046B1 (en) * 1999-06-02 2003-03-04 Akg Of America, Inc. Heat exchanger, particularly oil cooler
US6779591B2 (en) * 2000-08-25 2004-08-24 Modine Manufacturing Company Compact heat exchanger for a compact cooling system
US20060032626A1 (en) * 2002-07-04 2006-02-16 Keen Mark G Device for heat exchange between flowable media
WO2004005832A1 (en) * 2002-07-04 2004-01-15 Hydac S.A. Device for heat exchange between flowable media
CN100416213C (en) * 2002-07-04 2008-09-03 Hydac股份有限公司 Device for heat exchange between flowing media
US20040112577A1 (en) * 2002-09-12 2004-06-17 Ralf Beck Radiator with side flat tubes
US6904965B2 (en) * 2002-09-12 2005-06-14 Modine Manufacturing Company Radiator with side flat tubes
US8225849B2 (en) * 2003-10-02 2012-07-24 Behr Gmbh & Co. Kg Charge intercooler for a motor vehicle
US20070175612A1 (en) * 2003-10-02 2007-08-02 Behr Gmbh & Co. Kg Charge intercooler for a motor vehicle
US20050126517A1 (en) * 2003-12-12 2005-06-16 Visteon Global Technologies, Inc. Integrated heat exchange and fluid control device
US6997143B2 (en) * 2003-12-12 2006-02-14 Visteon Global Technologies, Inc. Integrated heat exchange and fluid control device
US7490662B2 (en) * 2004-10-13 2009-02-17 Visteon Global Technologies, Inc. Integrated thermal bypass valve
US20060076129A1 (en) * 2004-10-13 2006-04-13 Visteon Global Technologies, Inc. Integrated thermal bypass valve
US20120125594A1 (en) * 2010-11-18 2012-05-24 Hamilton Sundstrand Corporation Heat Exchanger System
US9658005B2 (en) * 2010-11-18 2017-05-23 Hamilton Sundstrand Corporation Heat exchanger system
DE102014010632A1 (en) 2014-07-17 2016-01-21 Modine Manufacturing Company Soldered heat exchanger and manufacturing process
FR3060057A1 (en) * 2016-12-14 2018-06-15 Safran Aircraft Engines FLUIDIC CIRCUIT IN A TURBOMACHINE
WO2018109374A1 (en) * 2016-12-14 2018-06-21 Safran Aircraft Engines Fluid circuit in a turbine engine
CN110073081A (en) * 2016-12-14 2019-07-30 赛峰航空器发动机 Fluid circuit in turbogenerator
JP2020502413A (en) * 2016-12-14 2020-01-23 サフラン・エアクラフト・エンジンズ Fluid circuit of turbine engine
RU2747706C2 (en) * 2016-12-14 2021-05-13 Сафран Эйркрафт Энджинз Liquid circuit in gas turbine engine
US11066997B2 (en) 2016-12-14 2021-07-20 Safran Aircraft Engines Fluid circuit in a turbine engine

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