US2083611A - Cooling system - Google Patents
Cooling system Download PDFInfo
- Publication number
- 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
- Authority
- US
- United States
- Prior art keywords
- liquid
- condenser
- heat
- cooling
- temperature
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P3/00—Liquid cooling
- F01P3/22—Liquid cooling characterised by evaporation and condensation of coolant in closed cycles; characterised by the coolant reaching higher temperatures than normal atmospheric boiling-point
- F01P3/2285—Closed cycles with condenser and feed pump
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B23/00—Machines, plants or systems, with a single mode of operation not covered by groups F25B1/00 - F25B21/00, e.g. using selective radiation effect
- F25B23/006—Machines, 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-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
- F28D15/02—Heat-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-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
- F28D15/02—Heat-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
- F28D15/0266—Heat-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-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
- F28D15/02—Heat-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
- F28D15/06—Control 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.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US579159A US2083611A (en) | 1931-12-05 | 1931-12-05 | Cooling system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US579159A US2083611A (en) | 1931-12-05 | 1931-12-05 | Cooling system |
Publications (1)
Publication Number | Publication Date |
---|---|
US2083611A true US2083611A (en) | 1937-06-15 |
Family
ID=24315795
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US579159A Expired - Lifetime US2083611A (en) | 1931-12-05 | 1931-12-05 | Cooling system |
Country Status (1)
Country | Link |
---|---|
US (1) | US2083611A (en) |
Cited By (81)
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 |
EP0141363A2 (en) * | 1983-10-26 | 1985-05-15 | Nissan Motor Co., Ltd. | Intercooler for supercharged internal combustion 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 |
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 |
-
1931
- 1931-12-05 US US579159A patent/US2083611A/en not_active Expired - Lifetime
Cited By (109)
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 |
EP0117349A3 (en) * | 1982-12-03 | 1985-01-09 | Mitsubishi Denki Kabushiki Kaisha | Cooling apparatus for an electrical transformer |
EP0117349A2 (en) * | 1982-12-03 | 1984-09-05 | 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 |
EP0141248A2 (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 |
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 |
EP0140162A2 (en) * | 1983-10-28 | 1985-05-08 | Nissan Motor Co., Ltd. | Improved cooling system for automotive 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 |
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 |
EP0182340A3 (en) * | 1984-11-20 | 1986-11-20 | Nissan Motor Co., Ltd. | Cooling system for automotive internal combustion engine or the like |
EP0182340A2 (en) * | 1984-11-20 | 1986-05-28 | 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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2083611A (en) | Cooling system | |
US3041842A (en) | System for supplying hot dry compressed air | |
US2292946A (en) | Vapor cooling system | |
US4353323A (en) | Apparatus for the treating of articles | |
US4361524A (en) | Cooling tower with plume prevention system | |
US2713995A (en) | Air heating and cooling system | |
US2327451A (en) | Air conditioner | |
US2320432A (en) | Refrigerating apparatus | |
US2091159A (en) | Means for dissipating heat from radiators containing liquid | |
EP3018433A1 (en) | System and method for providing air-cooling, and related power generation systems | |
US2064609A (en) | Method and apparatus for cooling liquids | |
US3385348A (en) | Heat exchanger unit | |
US3001379A (en) | Heat transfer system | |
US2308079A (en) | Refrigerating apparatus | |
US1376086A (en) | Automatic cooling system | |
US2239886A (en) | Power plant refrigerating system | |
US3161029A (en) | Refrigeration systems operable at low condenser pressures | |
US2005611A (en) | Dry ice refrigerating system | |
US4282926A (en) | Cooling of fluid streams | |
US2664001A (en) | Air cycle water cooler | |
US2023444A (en) | Air conditioning for moving vehicles | |
US2738653A (en) | Concentration control for absorption refrigerating system | |
USRE18826E (en) | And one-third to james e | |
US2085942A (en) | Refrigerating apparatus | |
US1954949A (en) | Air cooling and air conditioning device |