US3255740A - Engine coolant deaeration system - Google Patents

Engine coolant deaeration system Download PDF

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US3255740A
US3255740A US397525A US39752564A US3255740A US 3255740 A US3255740 A US 3255740A US 397525 A US397525 A US 397525A US 39752564 A US39752564 A US 39752564A US 3255740 A US3255740 A US 3255740A
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valve
tank
jacket
engine
conduit means
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US397525A
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John W Walsh
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Motors Liquidation Co
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Motors Liquidation Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P11/00Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
    • F01P11/02Liquid-coolant filling, overflow, venting, or draining devices
    • F01P11/028Deaeration devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P7/00Controlling of coolant flow
    • F01P7/14Controlling of coolant flow the coolant being liquid
    • F01P7/16Controlling of coolant flow the coolant being liquid by thermostatic control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04Cooling of air intake supply
    • F02B29/0406Layout of the intake air cooling or coolant circuit
    • F02B29/0437Liquid cooled heat exchangers
    • F02B29/0443Layout of the coolant or refrigerant circuit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P2060/00Cooling circuits using auxiliaries
    • F01P2060/02Intercooler
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P2060/00Cooling circuits using auxiliaries
    • F01P2060/08Cabin heater
    • 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

Definitions

  • An object of the present invention is to provide an engine coolant deaeration system in which one tank of a radiator is enabled to serve as a deaeration tank as engine temperature control is automatically maintained under a wide range of ambient temperature conditions and with avoidance of any carefully sized or balanced deaeration lines or bafiles.
  • a feature of the present invention is an engine coolant deaeration system in which one tank of a radiator at all times serves to provide a zone for the removal of air or gases from a coolant regardless of Whether or not the radiator core is bypassed by a thermostatic valve.
  • FIGURE 1 is a diagramatic view, in perspective, of a portion of a V-8 engine jacket associated with a radiator heater, a two-way thermostatic valve, an oil cooler and a Water pump;
  • FIGURE 2 is an enlarged sectional view looking in the direction of the arrows 22 through the thermostatic valve of FIGURE 1;
  • FIGURE 3 is a view similar to that of FIGURE 2 but with a main valve and a bypass valve each partially opened;
  • FIGURE 4 is a view similar to that of FIGURES 2 and 3 but with the main valve fully opened and the bypass valve closed.
  • FIGURE 1 The portion of a V-8 engine jacket is shown in FIGURE 1 as associated with a conventional radiator 12 which comprises a top or deaeration tank 14 and a bottom or second tank 16.
  • the tank 14 is provided with a conventional filler neck 18 having a pressure cap 20 and a vent line 22.
  • a suitable filler neck and pressure cap is disclosed in the United States Patent 3,047,235 granted July 31, 1962 in the name of I. Eshbaugh and I. Mc- Dougal.
  • a themostat valve 24 is shown at the junction of three conduits 26, 28, and and this valve is also connected by the latter to the inlet side of an air cooler 32.
  • the coolant outlet side of the latter is connected by means of an elbow 34 to the coolant pump 36.
  • the discharge side of the pump 36 is connected to the engine jacket 10.
  • a heater core 40 for heating the passenger compartment of the vehicle is connected to the engine jacket 10 by a conduit 42 and to the inlet side of the pump by a conduit 44.
  • This heater core or the oil cooler 32 forms no part of the present invention but each is shown in a preferred arrangement with the particular embodiment of the cooling system illustrated.
  • the dis charge of the jacket 10 is connected by a conduit 46 to the deaeration or upper tank 14 of the radiator 12.
  • the thermostatic valve 24 comprises two casing parts 50 and 52 between which is interposed a gasket 54.
  • This gasket surrounds an inserted annular valve seat 56 which is tightly held in the part 52 of the valve and a spider portion of which slidingly holds a plunger of a main valve 58.
  • the latter is movable to closed and opened positions with relation to the annular seat member 56 and a pellet motor casing 59 is firmly held in fixed relation to the seat member by means not shown.
  • the casing part 50 of the valve 24 defines an annular inlet chamber 60 connected by radial passages 62 to a central passage 64 and the latter is in alignment with the main valve 58.
  • the annular chamber 60 is connected to a neck 70 which in turn is adapted to be connected by a suitable coupling to one end of the conduit 28.
  • the upstream side of the main valve 58 is connected by a neck 72 to the conduit 26 leading from the bottom tank 16. Further details regarding the valve 24 are not given here as they form no part of the present invention. It sufiices to say, however, that heat opens the main valve 58 and closes a bypass or secondary valve 73 controlling the passages 62.
  • a suitable thermostatic valve is disclosed in the United States Patent 2,899,026, Hitch et al. or in United States Patent 2,988,068, Waydak.
  • the main valve 58 of the thermostat 24 When the main valve 58 of the thermostat 24 is atfull closed position, as shown in FIGURE 2, the total coolant flow is from the radiator top tank 14 and through the conduit 28 to the annular chamber 60 and then by Way of radial ports 62 to the chamber 64 and the line 30 back to the engine jacket. As the main valve is closed, there is no flow of coolant through the radiator core and although at this time the engine is cold, any gases forming in the coolant are promptly deaerated from the upper tank 14 by way of the pressure cap 20 and the vent 22. The tank 14 provides adequate opportunity for entrained gas to separate and baffles are not necessary.
  • the main valve 58 partially opens and the bypass valve 73 partially closes as shown in FIGURE 3.
  • a controlled engine or system temperature then exists wherein some coolant flowsthrough the radiator core and the remainder flows through bypass line 28 with deaeration being effected in the tank 14 from the complete flow.
  • the main valve 58 Will be fully opened and all the coolant flows through the radiator core and the conduit 26 giving the maximum cooling efiect.
  • the top tank 14 is effective to remove any entrapped gases from the coolant with no supplementary tanks being needed.
  • bypass conduit 28 is preferably connected as loW as possible to the top tank 14 and at a distance from the connection of the conduit 46. This separation of the points of joinder of conduits 46 and 28 to the top tank 14 permits adequate separation of the gas from the coolant.
  • the fittings for the heater core 40 are located in lower places in the system where small coolant flow turbulence occurs.
  • An engine coolant deaeration system comprising an engine jacket, a radiator with a top tank and a bottom tank, a pump, atwo-way thermostatic valve, first conduit means connecting said bottom tank to said valve, pump and jacket in series and in that order, second conduit means connecting said jacket, top tank and valve in series and in that order, the points of joinder of said second conduit means to said top tank being spaced to facilitate separation of gas, and the valve being such as to make said first conduit means effective when said jacket is heated and to make said second conduit means effective when said jacket is not heated.
  • An engine coolant deaeration system comprising an engine jacket, a radiator with a deaeration tank connected to a second tank by a core, a pump, a two-way thermostatic valve, first conduit means connecting said tank to said valve, pump and jacket in series and in that order,
  • second conduit means connecting said jacket, deaeration tank and valve in series and in that order, and the valve being such as to effect flow through the radiator and said first conduit means when said jacket is heated and to elfect flow through the second conduit means around said core to said pump when said jacket is not heated.
  • An engine coolant deaeration system comprising an engine jacket, a radiator with a deaeration tank connected to a second tank by a core, a pump, a two-way thermostatic valve, a vent on said deaeration tank, first conduit means cooperating in connecting said second tank to one way of said valve, said pump and said jacket in series,
  • second conduit means cooperating in connecting said jacket, deaeration tank and the other way of said valve in series, and the system being such that any fiow under any condition in said system is through said deaeration tank.
  • An engine coolant deaeration system comprising an engine jacket, a radiator with an upper tank and a lower tank connected by a core, a pump, a two-way thermostatic valve, a vent on said upper tank, first conduit means cooperating in connecting said lower tank to one way of said valve, said pump and said jacket in series, second conduit means cooperating in connecting said jacket, upper tank and the other way of said valve in series, and. the arrangement being such that all fiow through said thermostatic valve is from said upper tank.
  • thermostatic valve including a main valve controlling the fiow through said core and a bypass valve controlling the flow around said core to said pump.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)

Description

June 14, 1966 J. w. WALSH ENGINE COOLANT DEAERATION SYSTEM Filed Sept. 18, 1964 ldflwwwwwww INVENTOR. 19/211 (1/ Milk/1 7 OzQ/Vi'y United States Patent 3,255,740 ENGINE CODLANT DEAERATION SYSTEM John W. Walsh, Lockport, N.Y., assignor to General Motors Corporation, Detroit,-Mich., a corporation of Delaware Filed Sept. 18, 1964, Ser. No. 397,525 Claims. (Cl. 123-4109) This invention relates to engine cooling systems and more particularly to systems for cooling internal combustion engines by means of a circulatory liquid.
Internal combustion engines and particularly diesel engines are susceptible to the entry of combustion gases into the cooling systems causing the water or coolant pumps to become air locked. The entrainment of air or combustion gases in a coolant in other ways detracts from the desired efficiency of a given engine cooling system and it is obvious that an improved efiective and simple way for removing gases from engine coolants is desirable while retaining control of engine temperatures. The difliculty is much more serious with diesel engines as distinguished from other engines. The attempted solution in that case has been the customary one neve1thelessto add bleed holes in the thermostat but this expediency causes loss of coolant temperature control so that radiator shutters are needed to keep coolant leakage flowing in the radiator from becoming too cold under certain ambient conditions. Under low ambient temperature conditions, the conventional cooling systems tend to over-cool engines causing a loss in the latters efiiciency.
An object of the present invention is to provide an engine coolant deaeration system in which one tank of a radiator is enabled to serve as a deaeration tank as engine temperature control is automatically maintained under a wide range of ambient temperature conditions and with avoidance of any carefully sized or balanced deaeration lines or bafiles. v
To this end a feature of the present invention is an engine coolant deaeration system in which one tank of a radiator at all times serves to provide a zone for the removal of air or gases from a coolant regardless of Whether or not the radiator core is bypassed by a thermostatic valve.
This 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 a diagramatic view, in perspective, of a portion of a V-8 engine jacket associated with a radiator heater, a two-way thermostatic valve, an oil cooler and a Water pump;
FIGURE 2 is an enlarged sectional view looking in the direction of the arrows 22 through the thermostatic valve of FIGURE 1;
FIGURE 3 is a view similar to that of FIGURE 2 but with a main valve and a bypass valve each partially opened; and
FIGURE 4 is a view similar to that of FIGURES 2 and 3 but with the main valve fully opened and the bypass valve closed.
The portion of a V-8 engine jacket is shown in FIGURE 1 as associated with a conventional radiator 12 which comprises a top or deaeration tank 14 and a bottom or second tank 16. The tank 14 is provided with a conventional filler neck 18 having a pressure cap 20 and a vent line 22. A suitable filler neck and pressure cap is disclosed in the United States Patent 3,047,235 granted July 31, 1962 in the name of I. Eshbaugh and I. Mc- Dougal. A themostat valve 24 is shown at the junction of three conduits 26, 28, and and this valve is also connected by the latter to the inlet side of an air cooler 32. The coolant outlet side of the latter is connected by means of an elbow 34 to the coolant pump 36. The discharge side of the pump 36 is connected to the engine jacket 10. A heater core 40 for heating the passenger compartment of the vehicle is connected to the engine jacket 10 by a conduit 42 and to the inlet side of the pump by a conduit 44. This heater core or the oil cooler 32 forms no part of the present invention but each is shown in a preferred arrangement with the particular embodiment of the cooling system illustrated. The dis charge of the jacket 10 is connected by a conduit 46 to the deaeration or upper tank 14 of the radiator 12.
The thermostatic valve 24 comprises two casing parts 50 and 52 between which is interposed a gasket 54. This gasket surrounds an inserted annular valve seat 56 which is tightly held in the part 52 of the valve and a spider portion of which slidingly holds a plunger of a main valve 58. The latter is movable to closed and opened positions with relation to the annular seat member 56 and a pellet motor casing 59 is firmly held in fixed relation to the seat member by means not shown. The casing part 50 of the valve 24 defines an annular inlet chamber 60 connected by radial passages 62 to a central passage 64 and the latter is in alignment with the main valve 58. The annular chamber 60 is connected to a neck 70 which in turn is adapted to be connected by a suitable coupling to one end of the conduit 28. The upstream side of the main valve 58 is connected by a neck 72 to the conduit 26 leading from the bottom tank 16. Further details regarding the valve 24 are not given here as they form no part of the present invention. It sufiices to say, however, that heat opens the main valve 58 and closes a bypass or secondary valve 73 controlling the passages 62. A suitable thermostatic valve is disclosed in the United States Patent 2,899,026, Hitch et al. or in United States Patent 2,988,068, Waydak.
When the main valve 58 of the thermostat 24 is atfull closed position, as shown in FIGURE 2, the total coolant flow is from the radiator top tank 14 and through the conduit 28 to the annular chamber 60 and then by Way of radial ports 62 to the chamber 64 and the line 30 back to the engine jacket. As the main valve is closed, there is no flow of coolant through the radiator core and although at this time the engine is cold, any gases forming in the coolant are promptly deaerated from the upper tank 14 by way of the pressure cap 20 and the vent 22. The tank 14 provides adequate opportunity for entrained gas to separate and baffles are not necessary.
As the engine becomes warm and the thermostat 24 operates to control the engine temperature, the main valve 58 partially opens and the bypass valve 73 partially closes as shown in FIGURE 3. A controlled engine or system temperature then exists wherein some coolant flowsthrough the radiator core and the remainder flows through bypass line 28 with deaeration being effected in the tank 14 from the complete flow.
When the bypass valve 73 is fully closed as shown in FIGURE 4, the main valve 58 Will be fully opened and all the coolant flows through the radiator core and the conduit 26 giving the maximum cooling efiect. Under this heated engine condition as during the controlled flow condition, the top tank 14 is effective to remove any entrapped gases from the coolant with no supplementary tanks being needed.
It should be noted that the bypass conduit 28 is preferably connected as loW as possible to the top tank 14 and at a distance from the connection of the conduit 46. This separation of the points of joinder of conduits 46 and 28 to the top tank 14 permits adequate separation of the gas from the coolant. The fittings for the heater core 40 are located in lower places in the system where small coolant flow turbulence occurs.
I claim:
1. An engine coolant deaeration system comprising an engine jacket, a radiator with a top tank and a bottom tank, a pump, atwo-way thermostatic valve, first conduit means connecting said bottom tank to said valve, pump and jacket in series and in that order, second conduit means connecting said jacket, top tank and valve in series and in that order, the points of joinder of said second conduit means to said top tank being spaced to facilitate separation of gas, and the valve being such as to make said first conduit means effective when said jacket is heated and to make said second conduit means effective when said jacket is not heated.
2. An engine coolant deaeration system comprising an engine jacket, a radiator with a deaeration tank connected to a second tank by a core, a pump, a two-way thermostatic valve, first conduit means connecting said tank to said valve, pump and jacket in series and in that order,
second conduit means connecting said jacket, deaeration tank and valve in series and in that order, and the valve being such as to effect flow through the radiator and said first conduit means when said jacket is heated and to elfect flow through the second conduit means around said core to said pump when said jacket is not heated.
3. An engine coolant deaeration system comprising an engine jacket, a radiator with a deaeration tank connected to a second tank by a core, a pump, a two-way thermostatic valve, a vent on said deaeration tank, first conduit means cooperating in connecting said second tank to one way of said valve, said pump and said jacket in series,
second conduit means cooperating in connecting said jacket, deaeration tank and the other way of said valve in series, and the system being such that any fiow under any condition in said system is through said deaeration tank.
4. An engine coolant deaeration system comprising an engine jacket, a radiator with an upper tank and a lower tank connected by a core, a pump, a two-way thermostatic valve, a vent on said upper tank, first conduit means cooperating in connecting said lower tank to one way of said valve, said pump and said jacket in series, second conduit means cooperating in connecting said jacket, upper tank and the other way of said valve in series, and. the arrangement being such that all fiow through said thermostatic valve is from said upper tank.
5. An engine coolant deaeration system as set forth in claim 4, said thermostatic valve including a main valve controlling the fiow through said core and a bypass valve controlling the flow around said core to said pump.
References Cited by the Examiner UNITED STATES PATENTS 1,311,809 8/1919 Giesler 23634.5 2,296,641 9/1942 Hawkins l2341.1 2,332,680 10/1943 Wallace 12341.54 X 2,336,068 12/1943 Charles 12341.1 2,988,068 6/1961 Waydale 12341.1 3,014,467 12/1961 Middendorf l2341.1
KARL J. ALBRECHT, Primary Examiner.

Claims (1)

1. AN ENGINE COOLANT DEAERATION SYSTEM COMPRISING AN ENGINE JACKET, A RADIATOR WITH A TOP TANK AND A BOTTOM TANK, A PUMP, A TWO-WAY THERMOSTATIC VALVE, FIRST CONDUIT MEANS CONNECTING SAID BOTTOM TANK TO SAID VALVE, PUMP AND JACKET IN SERIES AND IN THAT ORDER, SECOND CONDUIT MEANS CONNECTING SAID JACKET, TOP TANK AND VALVE IN SERIES AND IN THAT ORDER, THE POINTS OF JOINDER OF SAID SECOND CONDUIT MEANS TO SAID TOP TANK BEING SPACED TO FACILITATE SEPARATION OF GAS, AND THE VALVE BEING SUCH AS TO MAKE SAID FIRST CONDUIT MEANS EFFECTIVE WHEN SAID JACKET IS HEATED AND TO MAKE SAID SECOND CONDUIT MEANS EFFECTIVE WHEN SAID JACKET IS NOT HEATED.
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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3326192A (en) * 1965-05-18 1967-06-20 John E Gerli Cooling system for internal combustion engines
US3648765A (en) * 1970-11-24 1972-03-14 Us Navy Temperature control system for space suit
US3759233A (en) * 1969-05-23 1973-09-18 Caterpillar Tractor Co Engine cooling system
US3946943A (en) * 1974-10-08 1976-03-30 Toyota Jidosha Kogyo Kabushiki Kaisha Cooling system of an internal combustion engine incorporating a by-pass flow control system
DE3112202A1 (en) * 1981-03-27 1982-10-14 Bayerische Motoren Werke Ag COOLING DEVICE FOR LIQUID-COOLED INTERNAL COMBUSTION ENGINES
US4807995A (en) * 1985-07-04 1989-02-28 Oem Messtechnik Gmbh Process for electro optical inspection of the mouth area of glass bottles
US5111774A (en) * 1989-09-25 1992-05-12 Mazda Motor Corporation Engine cooling system
US5727729A (en) * 1994-06-09 1998-03-17 Rover Group Limited Combined bypass and thermostat assembly
WO2003016689A1 (en) * 2001-08-16 2003-02-27 Segei Petrovich Terentiev Liquid cooling and heating system for an internal combustion engine
US20060060346A1 (en) * 2004-08-30 2006-03-23 Toyota Jidosha Kabushiki Kaisha Heat exchanger structure of automatic transmission
US20070074682A1 (en) * 2005-09-30 2007-04-05 Honda Motor Co., Ltd. Vehicular cooling system
US20090266311A1 (en) * 2008-04-29 2009-10-29 Ford Global Technologies, Llc Heat exchanger with integral thermostats
US20110005741A1 (en) * 2009-07-09 2011-01-13 Jeffrey Owen Sheppard Low Pressure Drop Thermal By-Pass Valve
WO2014081374A1 (en) * 2012-11-21 2014-05-30 Scania Cv Ab Thermostat for a cooling system which cools a combustion engine
EP2845635A1 (en) * 2013-09-10 2015-03-11 Vaillant GmbH Ventilator

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1311809A (en) * 1919-07-29 Cooling system fob internal-combustion engines
US2296641A (en) * 1940-09-27 1942-09-22 Chrysler Corp Engine water circulating system
US2332680A (en) * 1942-06-08 1943-10-26 John H Wallace Cooling system for liquid jacketed engines
US2336068A (en) * 1942-04-13 1943-12-07 Austin Motor Co Ltd Liquid cooling system for internal combustion engines
US2988068A (en) * 1960-07-22 1961-06-13 Gen Motors Corp Engine cooling system
US3014467A (en) * 1960-07-22 1961-12-26 Int Harvester Co Engine temperature regulating means

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1311809A (en) * 1919-07-29 Cooling system fob internal-combustion engines
US2296641A (en) * 1940-09-27 1942-09-22 Chrysler Corp Engine water circulating system
US2336068A (en) * 1942-04-13 1943-12-07 Austin Motor Co Ltd Liquid cooling system for internal combustion engines
US2332680A (en) * 1942-06-08 1943-10-26 John H Wallace Cooling system for liquid jacketed engines
US2988068A (en) * 1960-07-22 1961-06-13 Gen Motors Corp Engine cooling system
US3014467A (en) * 1960-07-22 1961-12-26 Int Harvester Co Engine temperature regulating means

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3326192A (en) * 1965-05-18 1967-06-20 John E Gerli Cooling system for internal combustion engines
US3759233A (en) * 1969-05-23 1973-09-18 Caterpillar Tractor Co Engine cooling system
US3648765A (en) * 1970-11-24 1972-03-14 Us Navy Temperature control system for space suit
US3946943A (en) * 1974-10-08 1976-03-30 Toyota Jidosha Kogyo Kabushiki Kaisha Cooling system of an internal combustion engine incorporating a by-pass flow control system
DE3112202A1 (en) * 1981-03-27 1982-10-14 Bayerische Motoren Werke Ag COOLING DEVICE FOR LIQUID-COOLED INTERNAL COMBUSTION ENGINES
US4807995A (en) * 1985-07-04 1989-02-28 Oem Messtechnik Gmbh Process for electro optical inspection of the mouth area of glass bottles
US5111774A (en) * 1989-09-25 1992-05-12 Mazda Motor Corporation Engine cooling system
US5727729A (en) * 1994-06-09 1998-03-17 Rover Group Limited Combined bypass and thermostat assembly
WO2003016689A1 (en) * 2001-08-16 2003-02-27 Segei Petrovich Terentiev Liquid cooling and heating system for an internal combustion engine
US20060060346A1 (en) * 2004-08-30 2006-03-23 Toyota Jidosha Kabushiki Kaisha Heat exchanger structure of automatic transmission
US7665513B2 (en) * 2004-08-30 2010-02-23 Toyota Jidosha Kabushiki Kaisha Heat exchanger structure of automatic transmission
US20070074682A1 (en) * 2005-09-30 2007-04-05 Honda Motor Co., Ltd. Vehicular cooling system
US7673592B2 (en) * 2005-09-30 2010-03-09 Honda Motor Co., Ltd. Vehicular cooling system
US20090266311A1 (en) * 2008-04-29 2009-10-29 Ford Global Technologies, Llc Heat exchanger with integral thermostats
US8418931B2 (en) * 2008-04-29 2013-04-16 Ford Global Technologies, Llc Heat exchanger with integral thermostats
US20110005741A1 (en) * 2009-07-09 2011-01-13 Jeffrey Owen Sheppard Low Pressure Drop Thermal By-Pass Valve
US8991719B2 (en) * 2009-07-09 2015-03-31 Dana Canada Corporation Low pressure drop thermal by-pass valve
WO2014081374A1 (en) * 2012-11-21 2014-05-30 Scania Cv Ab Thermostat for a cooling system which cools a combustion engine
EP2845635A1 (en) * 2013-09-10 2015-03-11 Vaillant GmbH Ventilator

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