US2083611A - Cooling system - Google Patents

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US2083611A
US2083611A US579159A US57915931A US2083611A US 2083611 A US2083611 A US 2083611A US 579159 A US579159 A US 579159A US 57915931 A US57915931 A US 57915931A US 2083611 A US2083611 A US 2083611A
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liquid
condenser
heat
cooling
temperature
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US579159A
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Henry H Marshall
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Carrier Corp
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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
    • F01P3/00Liquid cooling
    • F01P3/22Liquid cooling characterised by evaporation and condensation of coolant in closed cycles; characterised by the coolant reaching higher temperatures than normal atmospheric boiling-point
    • F01P3/2285Closed cycles with condenser and feed pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B23/00Machines, plants or systems, with a single mode of operation not covered by groups F25B1/00 - F25B21/00, e.g. using selective radiation effect
    • F25B23/006Machines, plants or systems, with a single mode of operation not covered by groups F25B1/00 - F25B21/00, e.g. using selective radiation effect boiling cooling systems
    • 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
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • 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
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/0266Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers
    • 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
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/06Control arrangements therefor

Definitions

  • This invention relates to an improved method and apparatus for the removal of heat at one temperature and the dissipation of the removed heat at some lower temperature.
  • the general object of the invention is to provide for the absorption of heat at a desired temperature, the absorbing medium being adapted to carry the heat to ,a point at which it is then dissipated to the atmosphere, or other- 10 wise, at a lower temperature.
  • Another object of the invention is to provide means for controlling, within desired limits, the higher temperature at which this heat is absorbed, regardless of variations in the lower 15 temperature at which the heat is subsequently dissipated.
  • a suitable medium such as dichloromethane or dichloroethylene, or other refrigerants 2 having related characteristics.
  • This refrigerant is circulated about an apparatus to be cooled, and since its inherent characteristics enable it to be converted from liquid to vapor state, at comparatively slight pressures, exceedingly 25 rapid and eflicient heat exchange will take place in carrying on cooling operations, even at comparatively low temperatures.
  • the refrigerant in absorbing heat, will be converted into, a vapor.
  • this vapor would then be compressed, and after the compression operation, would be subjected to condenser action in which the vapor would be reconverted into liquid form.
  • a refrigerant such as dichloromethane could be circulated about a cylinder, of a gas engine, for example, remove 45 heat therefrom, and in consequence, be converted, by evaporation. to a vapor.
  • the vapor would then proceed to a condenser, cooled by water, or by air, the cooling step reconverting the refrigerant to liquid form.
  • the liquid may 50 then be returned to the cylinder and the operation repeated.
  • a feature of the invention resides in the provision of a condenser employed. for converting refrigerant from vaporous to liquid state and 55 means for governing the condenser action so that the rate of conversion of refrigerant to liquid state may be accomplished at a predetermined rate.
  • Another feature resides in the control of the temperature of an object to be cooled by means of a condenser adapted to convert refrigerant used in the cooling operation from vaporous to liquid form, the condenser being adapted to regulate the pressure at which said refrigerant is converted from liquid to vaporous form.
  • Another feature resides in using a refrigerant as a heat absorption medium in a closed cooling circuit, the circuit adapted to be sealed, and the cooling operation adapted to be efficiently carried on even though the amount of refrigerant remains constant under all operating conditions.
  • Fig. 2 shows another form of my cooling arrangement illustrating a different method of control
  • Figs. 3, 4, and 5 illustrate modified forms of applying the invention in the accomplishment of controlled cooling operations
  • Fig. 6 shows the cooling system applied internal combustion engine
  • Fig. 7 is a section of part of the cooling system of Fig. 6.
  • This device may operate responsive to changes in temperature or in pressure within jacket 2, and regulate the entrance of condenser cooling liquid to line 8.
  • the arrangement of Fig. 1 will preferably operate with a. refrigerant within the jacket, such as dichloromethane. Others, however, having similar or related characteristics, such as dichloroethylene, may also be used.
  • a. refrigerant within the jacket such as dichloromethane.
  • some of the refrigerant liquid will evaporate, thus causing a transfer of heat from the chamber to the liquid.
  • the vapor will then rise and enter condenser 5 through whose tubes 6 comparatively cold water will be circulating.
  • the vapor will thereupon be condensed and drop back within the jacket.
  • the control device ll responds, as, for example, if it is a thermostatic device, to changes in .temperature within the jacket.
  • valve ID when more heat is generated in area I, it will cause more water to pass through valve l0 and enter condenser 5, whereas, whenless heat is given off, valve ID will correspondingly be controlled to admit less water within the condenser.
  • the condensing action is regulated responsive to variations in heat load produced within area I. Area I will, therefore, be maintained substantially at constant temperature.
  • the device ll instead of being responsive to changes in temperature, may react similarly to changes in pressure. The result, however, will be the same.
  • Fig. 2 illustrates a more comprehensive method of applying the cooling arrangement shown in Fig. 1.
  • Area I has a similar jacket 2 containing a heat transfer medium such as dichloromethane 3.
  • the condenser 5 in this case is air cooled, instead of water cooled. Any suitable means, such as a fan, not shown, or natural circulation of air about the condenser may be relied upon to bring about the desired condenser cooling effect.
  • Valve I! at the discharge end of the condenser permits refrigerant in liquid form to leave the condenser, in controlled amounts. However, if valve [2 remains closed, liquid will be stored within the condenser and, in effect, reduce the effective conated under similar conditions.
  • valve [2 is under control of device l3, which responds to changes either in temperature or pressure within the jacket.
  • Reservoir I 4 receives liquid passing through valve (2 which may then fiow through line i 5 and enter the jacket under control of valve l6.
  • Valve IE is under control of device I! which may respond to changes in temperature (or pressure) within jacket 2. It is evident that'instead of having two devices [3 and l! for the control respectively of valves l2 and IE, only one device may be used, since both valves are similarly actu- Two devices are shown because, in practice, it may be desired to actuate one valve responsive to temperature changes, whereas the other valve could more efficiently be operated responsive to pressure changes. The operation, as in Fig.
  • valve I comprises the evaporation of refrigerant 3, due to the production of heat within the area I.
  • the vapor then passes to the condenser 5 and is reconverted into a liquid by an air cooling action.
  • the valve l2, responsive to its control device l3, will allow the condensate to pass through in the event the heat load calls for further cooling.
  • valve I! will remain shut and allow the liquid to accumulate within the condenser tubes, thus cutting down the effective condenser area and correspondingly reducing the condensing action. It may be noted that as the liquid refrigerant accumulates in the condenser, the pressure on the evaporating liquid will be increased, with a consequent reduction in evaporation.
  • Figs. 3, 4 and 5 illustrate modified forms of applying the invention, showing various methods of control.
  • damper 20 operates responsive to control i9, similarly situated as are controls i3 and IT in Fig. 2.
  • the damper motor l8 will, therefore, regulate the position of damper 20 within the passage connecting jacket 2 and condenser 5.
  • This damper in effect, regulates the pressure on the liquid in the jacket and thus controls therate of evaporation.
  • can draw liquid refrigerant through passage 22 from the condenser 5.
  • the pump discharges the liquid through passage 24, leading to spray deck 25 situated at the upper or discharge end of the jacket.
  • the pump operates continuously and a flood of spray, therefore, constantly serves the jacket and retains the walls wetted at all times.
  • the rate of evaporation will be controlled by responsive to the position of float valve 26 within reservoir 21.
  • the reservoir serves to accumulate condensate, and when it reaches a certain level, the float .valve will serve to actuate an electrical switch and close a related circuit for operating the pump.
  • a switch of any suitable design may be'used whose contacts may be closed when the float reaches one position, and broken when the float reaches another position. The. use of this control assures the main- 'tenance of a substantially constant level of liquid within the jacket. Damper 20, as in Fig.
  • Figs. 6 and 7 applicant illustrates a practical embodiment of his invention, in connection with the cooling of an automobile or internal combustion engine.
  • the internal combustion engine here illustrated takes the place oi area I shown in the other figures.
  • the engine may be of conventional design, and, per se. forms no part of the invention.
  • the cooling system may include the usual jackets about the cylinders and various other elements such as connections, pump. reservoir, and radiator.
  • takes the place of the condenser 5 shown in the other figures.
  • a suitable reservoir or receiving tank 32 is located in the bottom of the radiator.
  • a series of louvres 33 are suitably positioned in front of the radiatnr.
  • a fan 34 provided in the usual manner and operative from one,-of the shafts of the motor may be used to draw air through the "radiator and in contact with the tubes thereof, so that the cooling operation may be carried on even though the engine remains stationary.
  • the control motor 35 analogous in construction to the damper motor I8 of Figs. 3, 4 and 5, operative responsive to control device 36, shown on Fig. 6, regulates the position of louvres 33.
  • the temperature of the engine would be maintained substantially constant. It should be ob served that not only is the method of control peculiarly adapted to maintain desired constant temperature conditions, but the use of refrigerants such as dichloromethane has many other salutary advantages.
  • the refrigerant may be sealed in, so that in amount it always remains the same and yet its cooling effect can be varied, depending upon changes in rate of evaporation, controlled through regulation of the condenser action. The danger of freezing does not exist.
  • a method of regulating the temperature of an object to be cooled consisting in evaporating a liquid in contact with the object, condensing the resultant vapors, at substantially the same pressure as the pressure at which these vapors were formed, by causing a change in the sensible heat only of a cooling medium by passing the same in heat exchange relation with the vapors, returning the condensed liquid so that it may again contact with said object, and regulating the flow of cooling medium by variations in the amount of heat tobe dissipated.
  • a method of regulating the temperature of an object to be cooled consisting in wetting the surface of said object with a volatile fluid whereby the fluid is evaporated, condensing the resultant vapors, at substantially the same pressure as the pressure at which these vapors were formed, by continuously, and at all times, circulating a cooled medium in heat exchange relation with the vapors, and controlling the rate of condensation by regulating quantitatively the flow of cooling medium by the temperature of said fluid.
  • a method of cooling an object subjected to varying heat loads consisting in wetting the surface of said object with a volatile fluid whereby the fluid is evaporated, condensing the resultant vapors, at substantially the same pressure as the pressure at which the vapors were formed, by continuously causing a change in the sensible heat of a cooling medium by circulating the same in heat exchange relation with the vapors, and controlling the rate of condensation by regulating quantitatively the flow of cooling medium.

Description

June 15, 1937. H. H. MARSHALL 2,033,611
000mm SYSTEM Filed Dec. 5, 1951 2 Sheets-Sheet l June 15, 1937. H H, MARSHALL 2,083,611
COOLING SYSTEM Filed Dec. 5, 1931 2 Sheets-Sheet 2 k I Z; 5
Patented June 15, 1937 UNITED STATES.
PATENT OFFICE COOLING SYSTEM ware Application. December 5, 1931, Serial No. 579,159
5 Claims.
This invention relates to an improved method and apparatus for the removal of heat at one temperature and the dissipation of the removed heat at some lower temperature.
5 The general object of the invention is to provide for the absorption of heat at a desired temperature, the absorbing medium being adapted to carry the heat to ,a point at which it is then dissipated to the atmosphere, or other- 10 wise, at a lower temperature.
Another object of the invention is to provide means for controlling, within desired limits, the higher temperature at which this heat is absorbed, regardless of variations in the lower 15 temperature at which the heat is subsequently dissipated. j
In carrying out these objects, applicant employs a suitable medium. such as dichloromethane or dichloroethylene, or other refrigerants 2 having related characteristics. This refrigerant is circulated about an apparatus to be cooled, and since its inherent characteristics enable it to be converted from liquid to vapor state, at comparatively slight pressures, exceedingly 25 rapid and eflicient heat exchange will take place in carrying on cooling operations, even at comparatively low temperatures. In the heat exchange step, the refrigerant, in absorbing heat, will be converted into, a vapor. In the usual 30 refrigeration cycle, this vapor would then be compressed, and after the compression operation, would be subjected to condenser action in which the vapor would be reconverted into liquid form. Applicant, however, has conceived 35 that such compression is unnecessary in carrying on controlled cooling operations, where the temperature of the apparatus or medium to be cooled need not be lower than the temperature of the atmosphere or any desired medium 40 adapted to be employed in reconverting a refrigerant from vaporous to liquid form. In practical application, -therefore, a refrigerant such as dichloromethane could be circulated about a cylinder, of a gas engine, for example, remove 45 heat therefrom, and in consequence, be converted, by evaporation. to a vapor. The vapor would then proceed to a condenser, cooled by water, or by air, the cooling step reconverting the refrigerant to liquid form. The liquid may 50 then be returned to the cylinder and the operation repeated.
A feature of the invention resides in the provision of a condenser employed. for converting refrigerant from vaporous to liquid state and 55 means for governing the condenser action so that the rate of conversion of refrigerant to liquid state may be accomplished at a predetermined rate.
Another feature resides in the control of the temperature of an object to be cooled by means of a condenser adapted to convert refrigerant used in the cooling operation from vaporous to liquid form, the condenser being adapted to regulate the pressure at which said refrigerant is converted from liquid to vaporous form.
Still another feature resides in the provision of means in combination with. a condenser whereby the rate of evaporation of a refrigerant may be controlled and the condensation of said refrigerant also controlled.
Another feature resides in using a refrigerant as a heat absorption medium in a closed cooling circuit, the circuit adapted to be sealed, and the cooling operation adapted to be efficiently carried on even though the amount of refrigerant remains constant under all operating conditions.
Other features making for efliclency and economy in operation and accomplishingdesired methods of control by various means, including regulation of condenser cooling, adjustment of condenser surface. variation 'of evaporation and condenser pressures. and further advantages in structure and design in apparatus suitable for carrying out the invention, will be more apparent from the following description of the invention, to be read in connection with the accompanying drawings, showing illustrative forms of application, in which:
Fig. 1 is a diagrammatic view of a simple application of my invention,
Fig. 2 shows another form of my cooling arrangement illustrating a different method of control,
Figs. 3, 4, and 5 illustrate modified forms of applying the invention in the accomplishment of controlled cooling operations,
Fig. 6 shows the cooling system applied internal combustion engine, and
Fig. 7 is a section of part of the cooling system of Fig. 6.
Considering the drawings, more particularly Fig. 1, numeral 1 designates an area containing a source of heat. In practice, it may be a device, either electrical of mechanical, or a container in which a chemical process takes place, giving of! heat at a constant or varying rate. Area I is surrounded by a jacket 2, containing a heat transfer medium 3, shown in liquid form. The jacket is connected by passage l to condenser 5. The condenser is formed. preferably, of a number of tubes to an 6, having finned surface thereon to facilitate heat transfer. The tubes are connected at their opposite ends to headers l, suitably provided with supply and discharge lines, respectively designated B and 9. Valve H) in the supply line operates responsive to control device II. This device may operate responsive to changes in temperature or in pressure within jacket 2, and regulate the entrance of condenser cooling liquid to line 8. In practice, the arrangement of Fig. 1 will preferably operate with a. refrigerant within the jacket, such as dichloromethane. Others, however, having similar or related characteristics, such as dichloroethylene, may also be used. Upon the generation of heat within area i, some of the refrigerant liquid will evaporate, thus causing a transfer of heat from the chamber to the liquid. The vapor will then rise and enter condenser 5 through whose tubes 6 comparatively cold water will be circulating. The vapor will thereupon be condensed and drop back within the jacket. The control device ll responds, as, for example, if it is a thermostatic device, to changes in .temperature within the jacket. Thus, when more heat is generated in area I, it will cause more water to pass through valve l0 and enter condenser 5, whereas, whenless heat is given off, valve ID will correspondingly be controlled to admit less water within the condenser. As a result, the condensing action is regulated responsive to variations in heat load produced within area I. Area I will, therefore, be maintained substantially at constant temperature. The device ll, instead of being responsive to changes in temperature, may react similarly to changes in pressure. The result, however, will be the same.
Dichloromethane is preferred as a refrigerant because it is peculiarly adapted to achieve applicants desired results. Its stability under almost all conditions within practical limits, its nontoxic character, the fact that it is non-inflammable, and that it will not corrode or coat surfaces, make it ideal for use as a cooling medium in an arrangement such as illustrated in simple form, by Fig. 1. Of particular importance, however, is the fact that dichloromethane is a liquid at atmospheric pressure at normal temperatures, under F., and its escape from the system is of no moment, because it will resume the liquid form. Since it is non-inflammable, non-explosive and non-toxic, it will do no harm nor create any unsatisfactory conditions. Also, its operating characteristics require but comparatively slight pressure for its evaporation even at temperatures of several hundred degrees Farenheit, whereas, such refrigerants as ammonia or propane, under similar conditions, would require tremendous structures capable of withstanding pressures up to and exceeding one thousand pounds per square inch. Besides, such other refrigerants are both unstable, as well as dangerous.
Fig. 2 illustrates a more comprehensive method of applying the cooling arrangement shown in Fig. 1. Area I has a similar jacket 2 containing a heat transfer medium such as dichloromethane 3. The condenser 5 in this case is air cooled, instead of water cooled. Any suitable means, such as a fan, not shown, or natural circulation of air about the condenser may be relied upon to bring about the desired condenser cooling effect. Valve I! at the discharge end of the condenser permits refrigerant in liquid form to leave the condenser, in controlled amounts. However, if valve [2 remains closed, liquid will be stored within the condenser and, in effect, reduce the effective conated under similar conditions.
denser area. The operation of valve [2 is under control of device l3, which responds to changes either in temperature or pressure within the jacket. Reservoir I 4 receives liquid passing through valve (2 which may then fiow through line i 5 and enter the jacket under control of valve l6. Valve IE is under control of device I! which may respond to changes in temperature (or pressure) within jacket 2. It is evident that'instead of having two devices [3 and l! for the control respectively of valves l2 and IE, only one device may be used, since both valves are similarly actu- Two devices are shown because, in practice, it may be desired to actuate one valve responsive to temperature changes, whereas the other valve could more efficiently be operated responsive to pressure changes. The operation, as in Fig. 1, comprises the evaporation of refrigerant 3, due to the production of heat within the area I. The vapor then passes to the condenser 5 and is reconverted into a liquid by an air cooling action. The valve l2, responsive to its control device l3, will allow the condensate to pass through in the event the heat load calls for further cooling. However, if the temperature conditions within area I do not require lowering of temperature, valve I! will remain shut and allow the liquid to accumulate within the condenser tubes, thus cutting down the effective condenser area and correspondingly reducing the condensing action. It may be noted that as the liquid refrigerant accumulates in the condenser, the pressure on the evaporating liquid will be increased, with a consequent reduction in evaporation. As further cooling is required, due to increase in load, valve [2 will open and valve IE will also open, thus permitting liquid to flow from the condenser back to the jacket. Reservoir i 4 stores up excess liquid which is admitted by,valve I8, so that the liquid level within the jacket may be maintained substantially at a desired point. Valves i2 and I6, therefore, serve respectively to maintain the temperature of area I substantially constant by regulating the condenser action and the level of liquid within the jacket. Not only is the control of level in the jacket important from the standpoint of maintaining substantially constant temperatures. within the area but the maintenance of the jacket walls in wetted condition is highly desirable in effecting maximum heat 7 transfer.
Figs. 3, 4 and 5 illustrate modified forms of applying the invention, showing various methods of control. In Fig. 3, damper 20 operates responsive to control i9, similarly situated as are controls i3 and IT in Fig. 2. The damper motor l8 will, therefore, regulate the position of damper 20 within the passage connecting jacket 2 and condenser 5. This damper, in effect, regulates the pressure on the liquid in the jacket and thus controls therate of evaporation. Pump 2| can draw liquid refrigerant through passage 22 from the condenser 5. The pump discharges the liquid through passage 24, leading to spray deck 25 situated at the upper or discharge end of the jacket. The pump operates continuously and a flood of spray, therefore, constantly serves the jacket and retains the walls wetted at all times. The rate of evaporation, as already noted, will be controlled by responsive to the position of float valve 26 within reservoir 21. The reservoir serves to accumulate condensate, and when it reaches a certain level, the float .valve will serve to actuate an electrical switch and close a related circuit for operating the pump. A switch of any suitable design may be'used whose contacts may be closed when the float reaches one position, and broken when the float reaches another position. The. use of this control assures the main- 'tenance of a substantially constant level of liquid within the jacket. Damper 20, as in Fig. 3, is controlled by motor IS, in turn operative responsive to changes in conditions aifecting de- 'vice l9, and hence controls the rate of evaporation by governing the pressure on the liquid in the jacket. Check valve 28 is arranged to prevent the liquid flowing back to the pump from the jacket, whenever the-pump is inoperative.
Fig. 5 represents another variation in the method of control. Valve 29 is here under control of device 30 which responds, as in Figs. 3 and 4, either to changes in pressure or temperature within the jacket. When the temperature rises, as in the case of. an increasing load, device 30 will cause valve 29 to open and the pump 2| will thereupon supply liquid from reservoir 21 to the jacket. The pump is of the centrifugal type and hence may operate continuously, supplying liquid as requirements demand whenever the regulating device operates valve 29. This arrangement obviates the necessity for a controlled motor circuit, as, for example, shown in Fig. 4. The control of temperature w thin area i is, as in Figs. 3-and 4, carried on by damper which regulates the pressure on the liquid within the jacket and hence the rate of evaporation.
In Figs. 6 and 7, applicant illustrates a practical embodiment of his invention, in connection with the cooling of an automobile or internal combustion engine. In effect, the internal combustion engine here illustrated takes the place oi area I shown in the other figures. The engine may be of conventional design, and, per se. forms no part of the invention. The cooling system may include the usual jackets about the cylinders and various other elements such as connections, pump. reservoir, and radiator. The radiator 3| takes the place of the condenser 5 shown in the other figures. A suitable reservoir or receiving tank 32 is located in the bottom of the radiator. A series of louvres 33 are suitably positioned in front of the radiatnr. so that onrushing air responsive to the forward motion of the motor or vehicle in which the motor is located will pass through the tubes of the radiator in varying amount depending upon the position of the louvres. A fan 34 provided in the usual manner and operative from one,-of the shafts of the motor may be used to draw air through the "radiator and in contact with the tubes thereof, so that the cooling operation may be carried on even though the engine remains stationary. The control motor 35, analogous in construction to the damper motor I8 of Figs. 3, 4 and 5, operative responsive to control device 36, shown on Fig. 6, regulates the position of louvres 33. Thus, as the engine requires more cooling effect, control device 36 will cause the damper louvre control motor 35 to open louvres 33 wider, so that more air will pass over the tubes of the radiator, thereby producing greater cooling effect. Of course, whenever the engine speeds up, fan 34 and pump 31' are also speeded up. However, unless the heat were not dissipated fast enough, the louvres 33 would remain unafiected. However, if, as, for example, under a load, the engine did not speed up, but the amount of heat to be dissipated increased, the control 35 would be actuated and cause louvres 33 to function so that more air would pass the radiator tubes. Thus, by con trolling the condenser action in the radiator, the temperature of the engine would be maintained substantially constant. It should be ob served that not only is the method of control peculiarly adapted to maintain desired constant temperature conditions, but the use of refrigerants such as dichloromethane has many other salutary advantages. The refrigerant may be sealed in, so that in amount it always remains the same and yet its cooling effect can be varied, depending upon changes in rate of evaporation, controlled through regulation of the condenser action. The danger of freezing does not exist. Furthermore, but a small quantity of refrigerant is required, compared to the amount of water, for example, needed .to accomplish similar results; but the more important factor is that the condensing surface required with this refrigerant is much smaller than that of the conventional radiator of equal capacity. Also, the use of refrigerant such as dichloromethane would not rust the interior of the jackets, nor would ever require -replacement or inspection during the life of the engine.
While the invention is shown applied to an internal combustion engine, it is obvious that a cooling arrangement of similar design may be adapted in countless systems wherein the dissipation of heat and the maintenance of substantially constant temperatures is desired. The methods of control shown in the drawings are not to be construed as limiting, but merely as illustrative of the ways in which the invention may be applied.
It is intended that the foregoing description and the accompanying drawings be regarded as illustrative only and not in a limiting sense, ap-
plicant limiting himself only as indicated in the accompanying claims.
. What I claim is:
1. A method of maintaining constant the temperature of an object containing a source of heat consisting in surrounding said object with a liquid adapted to evaporate, and controlling the rate of evaporation by continually passing a condensing fluid in heat exchange relation with the vapors resulting from the evaporation of said liquid and quantitatively regulating the flow of condensing fluid.
2. A method of maintaining constant the temperature of an object containing a source of heat consisting in surrounding said object with a liquid adapted to evaporate, whereby said liquid is vaporized, condensing the resultant vapors, at substantially the same pressure as the pressure with which these vapors were formed, by passing a cooling medium in heat exchange relation with the vapors at all times, returning the condensate for re-evaporation, and quantitatively controlling the amount of cooling medium passed in heat exchange relation with said vapors by the temperature of said liquid.
3. A method of regulating the temperature of an object to be cooled consisting in evaporating a liquid in contact with the object, condensing the resultant vapors, at substantially the same pressure as the pressure at which these vapors were formed, by causing a change in the sensible heat only of a cooling medium by passing the same in heat exchange relation with the vapors, returning the condensed liquid so that it may again contact with said object, and regulating the flow of cooling medium by variations in the amount of heat tobe dissipated.
4. A method of regulating the temperature of an object to be cooled consisting in wetting the surface of said object with a volatile fluid whereby the fluid is evaporated, condensing the resultant vapors, at substantially the same pressure as the pressure at which these vapors were formed, by continuously, and at all times, circulating a cooled medium in heat exchange relation with the vapors, and controlling the rate of condensation by regulating quantitatively the flow of cooling medium by the temperature of said fluid.
5. A method of cooling an object subjected to varying heat loads consisting in wetting the surface of said object with a volatile fluid whereby the fluid is evaporated, condensing the resultant vapors, at substantially the same pressure as the pressure at which the vapors were formed, by continuously causing a change in the sensible heat of a cooling medium by circulating the same in heat exchange relation with the vapors, and controlling the rate of condensation by regulating quantitatively the flow of cooling medium.
HENRY Hi MARSHALL.
US579159A 1931-12-05 1931-12-05 Cooling system Expired - Lifetime US2083611A (en)

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Cited By (81)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2437332A (en) * 1944-01-01 1948-03-09 Honeywell Regulator Co Low-temperature test chamber
US2548325A (en) * 1947-03-11 1951-04-10 Maytag Co Self-basting oven
US2643282A (en) * 1949-04-13 1953-06-23 Albert D Greene Electronic equipment cooling means
US2667046A (en) * 1951-03-07 1954-01-26 Wade Engineering Ltd Cooler for gas leaving roots blowers
US2677937A (en) * 1949-09-21 1954-05-11 Sam P Jones Vaporizer
US2734096A (en) * 1956-02-07 Electric transformers and like
US2759987A (en) * 1952-04-12 1956-08-21 Westinghouse Electric Corp Cooling electrical apparatus
US2787889A (en) * 1955-08-15 1957-04-09 Boeing Co Aircraft compartment cooling mechanism
US2796632A (en) * 1954-08-18 1957-06-25 Frank W Egan & Company Plastic extruder with evaporative cooling system
US2831173A (en) * 1954-02-15 1958-04-15 Gen Electric Vaporization cooled stationary electrical induction apparatus
US2849523A (en) * 1952-08-16 1958-08-26 Westinghouse Electric Corp Electrical apparatus with vaporizable liquid coolant
US2858355A (en) * 1952-08-16 1958-10-28 Westinghouse Electric Corp Electrical apparatus
US2875263A (en) * 1953-08-28 1959-02-24 Westinghouse Electric Corp Transformer control apparatus
US2915296A (en) * 1955-04-07 1959-12-01 Olin Mathieson Heat exchanger
US2923759A (en) * 1955-01-10 1960-02-02 Northrop Corp Temperature controller
US2944405A (en) * 1955-10-27 1960-07-12 Union Tank Car Co Conservation arrangement
US2985707A (en) * 1956-04-16 1961-05-23 Raytheon Co Electrical cooling system
US3013730A (en) * 1958-11-05 1961-12-19 Bok Hendrik Frederik Spray painting apparatus
US3024298A (en) * 1958-07-10 1962-03-06 Raytheon Co Evaporative-gravity cooling systems
US3030077A (en) * 1959-07-13 1962-04-17 Loyd W Disler Integral ebullient cooler
US3067279A (en) * 1958-03-31 1962-12-04 Westinghouse Electric Corp Cooling means for conducting parts
US3086372A (en) * 1960-02-19 1963-04-23 Alco Products Inc Heat exchange means for space vehicles
US3092977A (en) * 1959-11-17 1963-06-11 Union Carbide Corp Control apparatus for low temperature refrigeration system
US3130290A (en) * 1961-01-04 1964-04-21 Yoder Co Rotary welding transformer
US3150245A (en) * 1957-09-13 1964-09-22 Westinghouse Electric Corp Liquefied gas circuit interrupters
US3174540A (en) * 1963-09-03 1965-03-23 Gen Electric Vaporization cooling of electrical apparatus
US3213934A (en) * 1962-07-02 1965-10-26 Usines Chanson Sa Des Cooling system for liquids used in machine tools and similar appliances
US3226941A (en) * 1963-10-31 1966-01-04 Charles D Snelling Klystron cooling system assembly
US3245463A (en) * 1959-09-10 1966-04-12 Babcock & Wilcox Co Fluid pressurizer
US3264589A (en) * 1963-09-03 1966-08-02 Gen Electric Transformer pockets for vaporized cooling
US3298431A (en) * 1965-01-11 1967-01-17 Comstock & Wescott Heat transfer system
US3380515A (en) * 1964-10-28 1968-04-30 Derritron Ltd Electromechanical vibrators
US3390541A (en) * 1965-04-09 1968-07-02 Plessey Co Ltd Equipment housing arrangements
US3404730A (en) * 1966-12-02 1968-10-08 Hughes Aircraft Co Temperature control arrangement
US3440376A (en) * 1966-03-14 1969-04-22 Westinghouse Electric Corp Low-temperature or superconducting vacuum circuit interrupter
US3461109A (en) * 1964-11-09 1969-08-12 Phillips Petroleum Co Process for the polymerization of conjugated dienes
US3476175A (en) * 1967-11-02 1969-11-04 Bell Telephone Labor Inc Vapor-phase cooling of electronic components
FR2126180A1 (en) * 1971-02-26 1972-10-06 Ibm
US3945433A (en) * 1971-10-06 1976-03-23 Stotz & Co. Vacuum vaporization apparatus for heating one or a number of separate liquids
US4015439A (en) * 1975-06-02 1977-04-05 Stauffer Chemical Company Cooling process for subambient and above ambient temperatures
US4027728A (en) * 1975-03-31 1977-06-07 Mitsubishi Denki Kabushiki Kaisha Vapor cooling device for semiconductor device
US4127163A (en) * 1976-08-18 1978-11-28 Bechtel International Corp. Freezer-sublimer for gaseous diffusion plant
US4216903A (en) * 1977-03-07 1980-08-12 Giuffre Anthony A Heat exchange system for recycling stack heat
US4260014A (en) * 1979-04-09 1981-04-07 International Telephone And Telegraph Corporation Ebullient cooled power devices
US4311131A (en) * 1977-12-19 1982-01-19 Sabat Faramarz M Evacuated heatpipe solar collector
US4314601A (en) * 1978-10-04 1982-02-09 Giuffre Anthony A Heat exchange system for recycling waste heat
US4318275A (en) * 1980-06-02 1982-03-09 Aluminum Company Of America Atmospheric thermal energy conversion system
EP0117349A2 (en) * 1982-12-03 1984-09-05 Mitsubishi Denki Kabushiki Kaisha Cooling apparatus for an electrical transformer
EP0140162A2 (en) * 1983-10-28 1985-05-08 Nissan Motor Co., Ltd. Improved cooling system for automotive engine or the like
EP0141248A2 (en) * 1983-10-26 1985-05-15 Nissan Motor Co., Ltd. Intercooler for supercharged internal combustion engine or the like
EP0141363A2 (en) * 1983-10-26 1985-05-15 Nissan Motor Co., Ltd. Intercooler for supercharged internal combustion engine or the like
EP0146057A2 (en) * 1983-12-02 1985-06-26 Nissan Motor Co., Ltd. Cooling system for automotive engine
EP0161687A2 (en) * 1984-05-18 1985-11-21 Nissan Motor Co., Ltd. Cooling system for automotive engine
EP0182340A2 (en) * 1984-11-20 1986-05-28 Nissan Motor Co., Ltd. Cooling system for automotive internal combustion engine or the like
EP0207354A2 (en) * 1985-07-05 1987-01-07 Nissan Motor Co., Ltd. Method and system for cooling automotive engines
EP0214389A2 (en) * 1985-09-06 1987-03-18 Nissan Motor Co., Ltd. Cooling system for automotive engine or the like
EP0219099A2 (en) * 1985-10-15 1987-04-22 Nissan Motor Co., Ltd. Cooling system for an internal combustion engine
EP0249467A1 (en) * 1986-06-11 1987-12-16 BRITISH TELECOMMUNICATIONS public limited company Evaporative cooling system
US4722304A (en) * 1986-01-10 1988-02-02 Nissan Motor Co., Ltd. Cooling system for automotive engine or the like
FR2669962A1 (en) * 1990-11-30 1992-06-05 Renault EVAPORATIVE COOLING PROCESS FOR INTERNAL COMBUSTION ENGINE AND IMPLEMENTATION DEVICE.
WO1997014925A1 (en) * 1995-10-17 1997-04-24 Marlow Industries, Inc. Thermoelectric device with evaporating/condensing heat exchanger
WO1999035402A1 (en) * 1997-12-30 1999-07-15 Ateliers Busch S.A. Cooling device
US6279336B1 (en) * 1997-04-04 2001-08-28 Grundl Und Hoffmann Gmbh Gesellschaft Fur Elektrotechnische Assembly for switching electrical power
US6866092B1 (en) * 1981-02-19 2005-03-15 Stephen Molivadas Two-phase heat-transfer systems
US20050172644A1 (en) * 2002-04-08 2005-08-11 Hengliang Zhang Loop-type thermosiphon and stirling refrigerator
US7077189B1 (en) * 2005-01-21 2006-07-18 Delphi Technologies, Inc. Liquid cooled thermosiphon with flexible coolant tubes
US20060162904A1 (en) * 2005-01-21 2006-07-27 Bhatti Mohinder S Liquid cooled thermosiphon for electronic components
US20060162903A1 (en) * 2005-01-21 2006-07-27 Bhatti Mohinder S Liquid cooled thermosiphon with flexible partition
US20060211364A1 (en) * 2001-08-01 2006-09-21 Friedrich Brotz Cooling system for motor vehicles and method for controlling at least one air mass flow through a radiator
US20060283579A1 (en) * 2005-06-15 2006-12-21 Debashis Ghosh Integrated liquid cooled heat sink for electronic components
US20080276605A1 (en) * 2007-05-09 2008-11-13 Denso Corporation Exhaust heat recovery device
US20090293461A1 (en) * 2006-06-08 2009-12-03 Denso Corporation Exhaust Heat Recovery Device
US20140138058A1 (en) * 2012-11-20 2014-05-22 Elwha Llc Heat pipe having a channeled heat transfer array
US20160109193A1 (en) * 2014-10-21 2016-04-21 Greenergy Products, Inc. Equipment and Method
US20170013744A1 (en) * 2013-02-01 2017-01-12 Dell Products, L.P. Techniques for controlling vapor pressure in an immersion cooling tank
US10966349B1 (en) * 2020-07-27 2021-03-30 Bitfury Ip B.V. Two-phase immersion cooling apparatus with active vapor management
US11448434B1 (en) 2018-11-01 2022-09-20 Booz Allen Hamilton Inc. Thermal management systems
US11561036B1 (en) 2018-11-01 2023-01-24 Booz Allen Hamilton Inc. Thermal management systems
US11644221B1 (en) 2019-03-05 2023-05-09 Booz Allen Hamilton Inc. Open cycle thermal management system with a vapor pump device
US11796230B1 (en) 2019-06-18 2023-10-24 Booz Allen Hamilton Inc. Thermal management systems
US11835270B1 (en) 2018-06-22 2023-12-05 Booz Allen Hamilton Inc. Thermal management systems

Cited By (109)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2734096A (en) * 1956-02-07 Electric transformers and like
US2437332A (en) * 1944-01-01 1948-03-09 Honeywell Regulator Co Low-temperature test chamber
US2548325A (en) * 1947-03-11 1951-04-10 Maytag Co Self-basting oven
US2643282A (en) * 1949-04-13 1953-06-23 Albert D Greene Electronic equipment cooling means
US2677937A (en) * 1949-09-21 1954-05-11 Sam P Jones Vaporizer
US2667046A (en) * 1951-03-07 1954-01-26 Wade Engineering Ltd Cooler for gas leaving roots blowers
US2759987A (en) * 1952-04-12 1956-08-21 Westinghouse Electric Corp Cooling electrical apparatus
US2849523A (en) * 1952-08-16 1958-08-26 Westinghouse Electric Corp Electrical apparatus with vaporizable liquid coolant
US2858355A (en) * 1952-08-16 1958-10-28 Westinghouse Electric Corp Electrical apparatus
US2875263A (en) * 1953-08-28 1959-02-24 Westinghouse Electric Corp Transformer control apparatus
US2831173A (en) * 1954-02-15 1958-04-15 Gen Electric Vaporization cooled stationary electrical induction apparatus
US2796632A (en) * 1954-08-18 1957-06-25 Frank W Egan & Company Plastic extruder with evaporative cooling system
US2923759A (en) * 1955-01-10 1960-02-02 Northrop Corp Temperature controller
US2915296A (en) * 1955-04-07 1959-12-01 Olin Mathieson Heat exchanger
US2787889A (en) * 1955-08-15 1957-04-09 Boeing Co Aircraft compartment cooling mechanism
US2944405A (en) * 1955-10-27 1960-07-12 Union Tank Car Co Conservation arrangement
US2985707A (en) * 1956-04-16 1961-05-23 Raytheon Co Electrical cooling system
US3150245A (en) * 1957-09-13 1964-09-22 Westinghouse Electric Corp Liquefied gas circuit interrupters
US3067279A (en) * 1958-03-31 1962-12-04 Westinghouse Electric Corp Cooling means for conducting parts
US3024298A (en) * 1958-07-10 1962-03-06 Raytheon Co Evaporative-gravity cooling systems
US3013730A (en) * 1958-11-05 1961-12-19 Bok Hendrik Frederik Spray painting apparatus
US3030077A (en) * 1959-07-13 1962-04-17 Loyd W Disler Integral ebullient cooler
US3245463A (en) * 1959-09-10 1966-04-12 Babcock & Wilcox Co Fluid pressurizer
US3092977A (en) * 1959-11-17 1963-06-11 Union Carbide Corp Control apparatus for low temperature refrigeration system
US3086372A (en) * 1960-02-19 1963-04-23 Alco Products Inc Heat exchange means for space vehicles
US3130290A (en) * 1961-01-04 1964-04-21 Yoder Co Rotary welding transformer
US3213934A (en) * 1962-07-02 1965-10-26 Usines Chanson Sa Des Cooling system for liquids used in machine tools and similar appliances
US3174540A (en) * 1963-09-03 1965-03-23 Gen Electric Vaporization cooling of electrical apparatus
US3264589A (en) * 1963-09-03 1966-08-02 Gen Electric Transformer pockets for vaporized cooling
US3226941A (en) * 1963-10-31 1966-01-04 Charles D Snelling Klystron cooling system assembly
US3380515A (en) * 1964-10-28 1968-04-30 Derritron Ltd Electromechanical vibrators
US3461109A (en) * 1964-11-09 1969-08-12 Phillips Petroleum Co Process for the polymerization of conjugated dienes
US3298431A (en) * 1965-01-11 1967-01-17 Comstock & Wescott Heat transfer system
US3390541A (en) * 1965-04-09 1968-07-02 Plessey Co Ltd Equipment housing arrangements
US3440376A (en) * 1966-03-14 1969-04-22 Westinghouse Electric Corp Low-temperature or superconducting vacuum circuit interrupter
US3404730A (en) * 1966-12-02 1968-10-08 Hughes Aircraft Co Temperature control arrangement
US3476175A (en) * 1967-11-02 1969-11-04 Bell Telephone Labor Inc Vapor-phase cooling of electronic components
FR2126180A1 (en) * 1971-02-26 1972-10-06 Ibm
US3945433A (en) * 1971-10-06 1976-03-23 Stotz & Co. Vacuum vaporization apparatus for heating one or a number of separate liquids
US4027728A (en) * 1975-03-31 1977-06-07 Mitsubishi Denki Kabushiki Kaisha Vapor cooling device for semiconductor device
US4015439A (en) * 1975-06-02 1977-04-05 Stauffer Chemical Company Cooling process for subambient and above ambient temperatures
US4127163A (en) * 1976-08-18 1978-11-28 Bechtel International Corp. Freezer-sublimer for gaseous diffusion plant
US4216903A (en) * 1977-03-07 1980-08-12 Giuffre Anthony A Heat exchange system for recycling stack heat
US4311131A (en) * 1977-12-19 1982-01-19 Sabat Faramarz M Evacuated heatpipe solar collector
US4314601A (en) * 1978-10-04 1982-02-09 Giuffre Anthony A Heat exchange system for recycling waste heat
US4260014A (en) * 1979-04-09 1981-04-07 International Telephone And Telegraph Corporation Ebullient cooled power devices
US4318275A (en) * 1980-06-02 1982-03-09 Aluminum Company Of America Atmospheric thermal energy conversion system
US6866092B1 (en) * 1981-02-19 2005-03-15 Stephen Molivadas Two-phase heat-transfer systems
EP0117349A2 (en) * 1982-12-03 1984-09-05 Mitsubishi Denki Kabushiki Kaisha Cooling apparatus for an electrical transformer
EP0117349A3 (en) * 1982-12-03 1985-01-09 Mitsubishi Denki Kabushiki Kaisha Cooling apparatus for an electrical transformer
EP0141363A2 (en) * 1983-10-26 1985-05-15 Nissan Motor Co., Ltd. Intercooler for supercharged internal combustion engine or the like
US4632178A (en) * 1983-10-26 1986-12-30 Nissan Motor Co., Ltd. Intercooler for supercharged internal combustion engine
EP0141248A2 (en) * 1983-10-26 1985-05-15 Nissan Motor Co., Ltd. Intercooler for supercharged internal combustion engine or the like
EP0141248A3 (en) * 1983-10-26 1986-06-11 Nissan Motor Co., Ltd. Intercooler for supercharged internal combustion engine or the like
EP0141363A3 (en) * 1983-10-26 1986-07-09 Nissan Motor Co., Ltd. Intercooler for supercharged internal combustion engine or the like
EP0140162A3 (en) * 1983-10-28 1986-05-28 Nissan Motor Co., Ltd. Improved cooling system for automotive engine or the like
EP0140162A2 (en) * 1983-10-28 1985-05-08 Nissan Motor Co., Ltd. Improved cooling system for automotive engine or the like
US4649869A (en) * 1983-10-28 1987-03-17 Nissan Motor Co., Ltd. Cooling system for automotive engine or the like
EP0146057A2 (en) * 1983-12-02 1985-06-26 Nissan Motor Co., Ltd. Cooling system for automotive engine
EP0146057A3 (en) * 1983-12-02 1986-10-22 Nissan Motor Co., Ltd. Cooling system for automotive engine
EP0161687A2 (en) * 1984-05-18 1985-11-21 Nissan Motor Co., Ltd. Cooling system for automotive engine
EP0161687A3 (en) * 1984-05-18 1986-11-20 Nissan Motor Co., Ltd. Cooling system for automotive engine
EP0182340A2 (en) * 1984-11-20 1986-05-28 Nissan Motor Co., Ltd. Cooling system for automotive internal combustion engine or the like
EP0182340A3 (en) * 1984-11-20 1986-11-20 Nissan Motor Co., Ltd. Cooling system for automotive internal combustion engine or the like
US4662318A (en) * 1984-11-20 1987-05-05 Nissan Motor Co., Ltd. Cooling system for automotive internal combustion engine or the like
EP0207354A3 (en) * 1985-07-05 1988-03-16 Nissan Motor Co., Ltd. Cooling system for automotive engine or the like
EP0207354A2 (en) * 1985-07-05 1987-01-07 Nissan Motor Co., Ltd. Method and system for cooling automotive engines
EP0214389A3 (en) * 1985-09-06 1988-03-30 Nissan Motor Co., Ltd. Cooling system for automotive engine or the like
EP0214389A2 (en) * 1985-09-06 1987-03-18 Nissan Motor Co., Ltd. Cooling system for automotive engine or the like
EP0219099A2 (en) * 1985-10-15 1987-04-22 Nissan Motor Co., Ltd. Cooling system for an internal combustion engine
EP0219099A3 (en) * 1985-10-15 1988-07-20 Nissan Motor Co., Ltd. Cooling system for automotive engine or the like
US4722304A (en) * 1986-01-10 1988-02-02 Nissan Motor Co., Ltd. Cooling system for automotive engine or the like
WO1987007706A1 (en) * 1986-06-11 1987-12-17 British Telecommunications Public Limited Company Evaporative cooling system
EP0249467A1 (en) * 1986-06-11 1987-12-16 BRITISH TELECOMMUNICATIONS public limited company Evaporative cooling system
FR2669962A1 (en) * 1990-11-30 1992-06-05 Renault EVAPORATIVE COOLING PROCESS FOR INTERNAL COMBUSTION ENGINE AND IMPLEMENTATION DEVICE.
EP0489628A1 (en) * 1990-11-30 1992-06-10 Regie Nationale Des Usines Renault S.A. Evaporative cooling method for an internal combustion engine and device for carrying out this method
US5737923A (en) * 1995-10-17 1998-04-14 Marlow Industries, Inc. Thermoelectric device with evaporating/condensing heat exchanger
US6003319A (en) * 1995-10-17 1999-12-21 Marlow Industries, Inc. Thermoelectric refrigerator with evaporating/condensing heat exchanger
WO1997014925A1 (en) * 1995-10-17 1997-04-24 Marlow Industries, Inc. Thermoelectric device with evaporating/condensing heat exchanger
US6279336B1 (en) * 1997-04-04 2001-08-28 Grundl Und Hoffmann Gmbh Gesellschaft Fur Elektrotechnische Assembly for switching electrical power
WO1999035402A1 (en) * 1997-12-30 1999-07-15 Ateliers Busch S.A. Cooling device
US6371742B1 (en) 1997-12-30 2002-04-16 Ateliers Busch S.A. Cooling device
US20060211364A1 (en) * 2001-08-01 2006-09-21 Friedrich Brotz Cooling system for motor vehicles and method for controlling at least one air mass flow through a radiator
US20050172644A1 (en) * 2002-04-08 2005-08-11 Hengliang Zhang Loop-type thermosiphon and stirling refrigerator
US20060162904A1 (en) * 2005-01-21 2006-07-27 Bhatti Mohinder S Liquid cooled thermosiphon for electronic components
US20060162898A1 (en) * 2005-01-21 2006-07-27 Ilya Reyzin Liquid cooled thermosiphon with flexible coolant tubes
US20060162903A1 (en) * 2005-01-21 2006-07-27 Bhatti Mohinder S Liquid cooled thermosiphon with flexible partition
US7077189B1 (en) * 2005-01-21 2006-07-18 Delphi Technologies, Inc. Liquid cooled thermosiphon with flexible coolant tubes
US7506682B2 (en) 2005-01-21 2009-03-24 Delphi Technologies, Inc. Liquid cooled thermosiphon for electronic components
US20060283579A1 (en) * 2005-06-15 2006-12-21 Debashis Ghosh Integrated liquid cooled heat sink for electronic components
US7604040B2 (en) * 2005-06-15 2009-10-20 Coolit Systems Inc. Integrated liquid cooled heat sink for electronic components
US20090293461A1 (en) * 2006-06-08 2009-12-03 Denso Corporation Exhaust Heat Recovery Device
US7946112B2 (en) * 2006-06-08 2011-05-24 Denso Corporation Exhaust heat recovery device
US20080276605A1 (en) * 2007-05-09 2008-11-13 Denso Corporation Exhaust heat recovery device
US7877991B2 (en) * 2007-05-09 2011-02-01 Denso Corporation Exhaust heat recovery device
US20140138058A1 (en) * 2012-11-20 2014-05-22 Elwha Llc Heat pipe having a channeled heat transfer array
US20170013744A1 (en) * 2013-02-01 2017-01-12 Dell Products, L.P. Techniques for controlling vapor pressure in an immersion cooling tank
US9844166B2 (en) * 2013-02-01 2017-12-12 Dell Products, L.P. Techniques for controlling vapor pressure in an immersion cooling tank
US20160109193A1 (en) * 2014-10-21 2016-04-21 Greenergy Products, Inc. Equipment and Method
US11835270B1 (en) 2018-06-22 2023-12-05 Booz Allen Hamilton Inc. Thermal management systems
US11448434B1 (en) 2018-11-01 2022-09-20 Booz Allen Hamilton Inc. Thermal management systems
US11561036B1 (en) 2018-11-01 2023-01-24 Booz Allen Hamilton Inc. Thermal management systems
US11561029B1 (en) 2018-11-01 2023-01-24 Booz Allen Hamilton Inc. Thermal management systems
US11644221B1 (en) 2019-03-05 2023-05-09 Booz Allen Hamilton Inc. Open cycle thermal management system with a vapor pump device
US11761685B1 (en) 2019-03-05 2023-09-19 Booz Allen Hamilton Inc. Open cycle thermal management system with a vapor pump device and recuperative heat exchanger
US11801731B1 (en) * 2019-03-05 2023-10-31 Booz Allen Hamilton Inc. Thermal management systems
US11835271B1 (en) 2019-03-05 2023-12-05 Booz Allen Hamilton Inc. Thermal management systems
US11796230B1 (en) 2019-06-18 2023-10-24 Booz Allen Hamilton Inc. Thermal management systems
US10966349B1 (en) * 2020-07-27 2021-03-30 Bitfury Ip B.V. Two-phase immersion cooling apparatus with active vapor management

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