US 7,708,053 B2Grant
Heat transfer system
Issue Date:2010-05-04
•20 Claims
•36 Drawing Sheets
Abstract
A thermodynamic system includes a cyclical heat exchange system and a heat transfer system coupled to the cyclical heat exchange system to cool a portion of the cyclical heat exchange system. The heat transfer system includes an evaporator including a wall configured to be coupled to a portion of the cyclical heat exchange system and a primary wick coupled to the wall and a condenser coupled to the evaporator to form a closed loop that houses a working fluid.
Metadata
Assignee
- Alliant Techsystems Inc.
Inventors
- Edward J. Kroliczek
- Michael Nikitkin
- David A. Wolf
Application Information
Application Number:US 10/694,387
Filing Date:2003-10-28
Priority Date:2000-06-30
Art Unit:3744
Classifications
IPC:
F28D15/00
Patent Drawings (36 sheets)
Description
Cross Reference to Related Applications
[0001] This application claims priority to U.S. Provisional Patent Application Ser. No. 60/421,737, filed Oct. 28, 2002, which is incorporated herein by reference.
[0002] This application also claims priority to U.S. Provisional Patent Application Ser. No. 60/514,670, titled “HEAT TRANSFER SYSTEM FOR A CYCLICAL HEAT EXCHANGE SYSTEM,” filed Oct. 28, 2003, which also is incorporated herein by reference.
[0003] This application is a continuation-in-part of U.S. patent application Ser. No. 10/676,265, titled “EVAPORATOR FOR A HEAT TRANSFER SYSTEM,” filed Oct. 2, 2003, which claimed priority to U.S. Patent Application Ser. No. 60/415,424, filed Oct. 2, 2002, which are also incorporated herein by reference.
[0004] This application is a continuation-in-part of U.S. patent application Ser. No. 10/602,022, filed Jun. 24, 2003, now U.S. Pat. No. 7,004,240, issued Feb. 28, 2006, which claims the benefit of U.S. Provisional Patent Application Ser. No. 60/391,006, filed Jun. 24, 2002 and is a continuation-in-part of U.S. patent application Ser. No. 09/896,561, filed Jun. 29, 2001, now U.S. Pat. No. 6,889,754, issued May 10, 2005, which claims the benefit of U.S. Provisional Patent Application Ser. No. 60/215,588, filed Jun. 30, 2000. All of these applications are incorporated herein by reference.
Technical Field
[0005] This description relates to heat transfer systems for use in cyclical heat exchange systems.
Background
[0006] Heat transfer systems are used to transport heat from one location (the heat source) to another location (the heat sink). Heat transfer systems can be used in terrestrial or extraterrestrial applications. For example, heat transfer systems may be integrated by satellite equipment that operates within zero- or low-gravity environments. As another example, heat transfer systems can be used in electronic equipment, which often requires cooling during operation.
[0007] Loop Heat Pipes (LHPs) and Capillary Pumped Loops (CPLs) are passive two-phase heat transfer systems. Each includes an evaporator thermally coupled to the heat source, a condenser thermally coupled to the heat sink, fluid that flows between the evaporator and the condenser, and a fluid reservoir for expansion of the fluid. The fluid within the heat transfer system can be referred to as the working fluid. The evaporator includes a primary wick and a core that includes a fluid flow passage. Heat acquired by the evaporator is transported to and discharged by the condenser. These systems utilize capillary pressure developed in a fine-pored wick within the evaporator to promote circulation of working fluid from the evaporator to the condenser and back to the evaporator. The primary distinguishing characteristic between an LHP and a CPL is the location of the loop's reservoir, which is used to store excess fluid displaced from the loop during operation. In general, the reservoir of a CPL is located remotely from the evaporator, while the reservoir of an LHP is co-located with the evaporator.
Summary
[0008] In one general aspect, a heat transfer system for a cyclical heat exchange system includes an evaporator including a wall configured to be coupled to a portion of the cyclical heat exchange system and a primary wick coupled to the wall and a condenser coupled to the evaporator to form a closed loop that houses a working fluid.
[0009] Implementations may include one or more of the following aspects. For example, the condenser includes a vapor inlet and a liquid outlet and the heat transfer system includes a vapor line providing fluid communication between the vapor outlet and the vapor inlet and a liquid return line providing fluid communication between the liquid outlet and the liquid inlet.
[0010] The evaporator includes a liquid barrier wall containing the working fluid on an inner side of the liquid barrier wall, which working fluid flows only along the inner side of the liquid barrier wall, wherein the primary wick is positioned between a heated wall and the inner side of the liquid barrier wall; a vapor removal channel that is located at an interface between the primary wick and the heated wall, the vapor removal channel extending to a vapor outlet; and a liquid flow channel located between the liquid barrier wall and the primary wick, the liquid flow channel receiving liquid from a liquid inlet.
[0011] The working fluid is moved through the heat transfer system passively.
[0012] The working fluid is moved through the heat transfer system without the use of external pumping.
[0013] The working fluid within the heat transfer system changes between a liquid and a vapor as the working fluid passes through or within one or more of the evaporator, the condenser, the vapor line, and the liquid return line.
[0014] The working fluid is moved through the heat transfer system passively.
[0015] The working fluid is moved through the heat transfer system with the use of the wick.
[0016] The heat transfer system further includes fins thermally coupled to the condenser to reject heat to an ambient environment.
[0017] In another general aspect, a thermodynamic system includes a cyclical heat exchange system and a heat transfer system coupled to the cyclical heat exchange system to cool a portion of the cyclical heat exchange system. The heat transfer system includes an evaporator including a wall configured to be coupled to a portion of the cyclical heat exchange system and a primary wick coupled to the wall and a condenser coupled to the evaporator to form a closed loop that houses a working fluid.
[0018] Implementations may include one or more of the following features. The evaporator is integral with the cyclical heat exchange system. The evaporator is thermally coupled to the portion of the cyclical heat exchange system. The cyclical heat exchange system includes a Stirling heat exchange system. The cyclical heat exchange system includes a refrigeration system. The heat transfer system is coupled to a hot side of the cyclical heat exchange system. The thermodynamic system heat transfer system is coupled to a cold side of the cyclical heat exchange system.
[0019] In another general aspect, a method utilizes the systems recited above.
[0020] The evaporator may be used in any two-phase heat transfer system for use in terrestrial or extraterrestrial applications. For example, the heat transfer systems can be used in electronic equipment, which often requires cooling during operation or in laser diode applications.
[0021] The planar evaporator may be used in any heat transfer system in which the heat source is formed as a planar surface. The annular evaporator may be used in any heat transfer system in which the heat source is formed as a cylindrical surface.
[0022] The heat transfer system that uses the annular evaporator may take advantage of gravity when used in terrestrial applications, thus making an LHP suitable for mass production. Terrestrial applications often dictate the orientation of the heat acquisition surfaces and the heat sink; the annular evaporator utilizes the advantages of the operation in gravity.
[0023] The heat transfer system provides a thermally efficient and space efficient system for cooling a cyclical heat exchange system because the evaporator of the heat transfer system is thermally and spatially coupled to a portion of the cyclical heat exchange system that is being cooled by the heat transfer system. For example, if the portion to be cooled (also known as a heat source) has a cylindrical geometry, the heat transfer system may include an annular evaporator. Use of the heat transfer system enables exploitation of cylindrical cyclical heat exchange systems, which are capable of being used in a commercially practical application for cabinet cooling.
[0024] Integral incorporation of the evaporator or condenser with the heat source of the cyclical heat exchange system can minimize packaging size. On the other hand, if the evaporator or condenser is clamped onto the heat source, the deployment and replacement of parts is facilitated.
[0025] The heat transfer system may be used to cool a cyclical heat exchange system having a cylindrical geometry, such as, for example, a free-piston Stirling cycle. A heat transfer system provides efficient fluid line connection (one vapor phase and on sub-cooled liquid return line connector) to and from an equally efficiently packaged annular condenser assembly.
[0026] The heat transfer system incorporates a condenser that is efficiently packaged as a flat plate condenser that is formed into annular sections to which are attached extended air heat exchange surface elements such as corrugated fin stock.
[0027] The heat transfer system combines efficient heat transfer mechanisms (evaporation and condensation) to couple the fluid of the Stirling cycle (helium) to the ultimate heat sink (ambient air). Consequently, a significant improvement in Stirling cycle efficiency (for example, up to 50%) is provided.
[0028] The evaporator and the condenser of the heat transfer system can be independently designed and optimized. This allows any number of attachment options to the cyclical heat exchange system. Moreover, the heat transfer system is insensitive to gravity orientation because a wick is incorporated into the evaporator.
[0029] The heat transfer system provides efficient cooling to a cabinet, such as a refrigerator or vending machine, in a small package at a commercially acceptable cost.
[0030] According to one implementation, an annular evaporator is clamped onto a cyclical heat exchange system and thermally coupled with thermal grease compound to provide easy assembly and servicing. According to another implementation, an annular evaporator is interference fit onto a cyclical heat exchange system to provide easy assembly with improved thermal efficiency. According to a further implementation, an annular evaporator is integrally formed with a cyclical heat exchange system to provide further improved thermal efficiency.
[0031] The heat transfer system includes a condenser having finned inner and outer annular portions to provide efficient heat transfer to the air in a reduced packaging space. The condenser may be roll bonded or formed by extrusion.
[0032] A loop heat pipe of the present invention provides for efficient packaging with a cylindrical refrigerator by adapting the traditional cylindrical geometry of a LHP evaporator to a planar “flat-plate” geometry that can be wrapped in an annular shape.
[0033] The packaging of the heat transfer system is described with respect to a few exemplary implementations, but is not meant to be limited to those exemplary implementations. Although described with respect to use for cooling a cabinet, such as a domestic refrigerator, vending machine, or point-of-sale refrigeration unit, one of skill in the art will recognize the numerous other useful applications of a compact, energy efficient and environmentally friendly refrigeration unit utilizing the heat transfer system as described herein.
[0034] Other features and advantages will be apparent from the description, the drawings, and the claims.
Description of Drawings
[0035] FIG. 1 is a schematic diagram of a heat transport system.
[0036] FIG. 2 is a diagram of an implementation of the heat transport system schematically shown by FIG. 1 .
[0037] FIG. 3 is a flow chart of a procedure for transporting heat using a heat transport system.
[0038] FIG. 4 is a graph showing temperature profiles of various components of the heat transport system during the process flow of FIG. 3 .
[0039] FIG. 5A is a diagram of a three-port main evaporator shown within the heat transport system of FIG. 1 .
[0040] FIG. 5B is a cross-sectional view of the main evaporator taken along 5B-5B of FIG. 5A .
[0041] FIG. 6 is a diagram of a four-port main evaporator that can be integrated into a heat transport system illustrated by FIG. 1 .
[0042] FIG. 7 is a schematic diagram of an implementation of a heat transport system.
[0043] FIGS. 8A , 8B, 9A, and 9B are perspective views of applications using a heat transport system.
[0044] FIG. 8C is a cross-sectional view of a fluid line taken along 8C-8C of FIG. 8A .
[0045] FIGS. 8D and 9C are schematic diagrams of the implementations of the heat transport systems of FIGS. 8A and 9A , respectively.
[0046] FIG. 10 is a cross-sectional view of a planar evaporator.
[0047] FIG. 11 is an axial cross-sectional view of an annular evaporator.
[0048] FIG. 12 is a radial cross-sectional view of the annular evaporator of FIG. 11 .
[0049] FIG. 13 is an enlarged view of a portion of the radial cross-sectional view of the annular evaporator of FIG. 12 .
[0050] FIG. 14A is a perspective view of the annular evaporator of FIG. 11 .
[0051] FIG. 14B is a top and partial cutaway view of the annular evaporator of FIG. 14A .
[0052] FIG. 14C is an enlarged cross-sectional view of a portion of the annular evaporator of FIG. 14B .
[0053] FIG. 14D is a cross-sectional view of the annular evaporator of FIG. 14B taken along line 14D-14D.
[0054] FIGS. 14E and 14F are enlarged views of portions of the annular evaporator of FIG. 14D .
[0055] FIG. 14G is a perspective cut-away view of the annular evaporator of FIG. 14A .
[0056] FIG. 14H is a detail perspective cut-away view of the annular evaporator of FIG. 14G .
[0057] FIG. 15A is a flat detail view of the heated wall formed into a shell ring component of the annular evaporator of FIG. 14A .
[0058] FIG. 15B is a cross-sectional view of the heated wall of FIG. 15A taken along line 15B-15B.
[0059] FIG. 16A is a perspective view of a primary wick of the annular evaporator of FIG. 14A .
[0060] FIG. 16B is a top view of the primary wick of FIG. 16A .
[0061] FIG. 16C is a cross-sectional view of the primary wick of FIG. 16B taken along line 16C-16C.
[0062] FIG. 16D is an enlarged view of a portion of the primary wick of FIG. 16C .
[0063] FIG. 17A is a perspective view of a liquid barrier wall formed into an annular ring of the annular evaporator of FIG. 14A .
[0064] FIG. 17B is a top view of the liquid barrier wall of FIG. 17A .
[0065] FIG. 17C is a cross-sectional view of the liquid barrier wall of FIG. 17B taken along line 17C-17C.
[0066] FIG. 17D is an enlarged view of a portion of the liquid barrier wall of FIG. 17C .
[0067] FIG. 18A is a perspective view of a ring separating the liquid barrier wall of FIG. 17A from the heated wall of FIG. 15A .
[0068] FIG. 18B is a top view of the ring of FIG. 18A .
[0069] FIG. 18C is a cross-sectional view of the ring of FIG. 18B taken along line 18C-18C.
[0070] FIG. 18D is an enlarged view of a portion of the ring of FIG. 18C .
[0071] FIG. 19A is a perspective view of a ring of the annular evaporator of FIG. 14A .
[0072] FIG. 19B is a top view of the ring of FIG. 19A .
[0073] FIG. 19C is a cross-sectional view of the ring of FIG. 19B taken along 19C-19C.
[0074] FIG. 19D is an enlarged view of a portion of the ring of FIG. 19C .
[0075] FIG. 20 is a perspective view of a cyclical heat exchange system that can be cooled using a heat transfer system.
[0076] FIG. 21 is a cross-sectional view of a cyclical heat exchange system such as the cyclical heat exchange system of FIG. 20 .
[0077] FIG. 22 is a side view of a cyclical heat exchange system such as the cyclical heat exchange system of FIG. 20 .
[0078] FIG. 23 is a schematic diagram of a first implementation of a cyclical heat exchange system including a cyclical heat exchange system and a heat transfer system.
[0079] FIG. 24 is a schematic diagram of a second implementation of a cyclical heat exchange system including a cyclical heat exchange system and a heat transfer system.
[0080] FIG. 25 is a schematic diagram of a heat transfer system using an evaporator designed in accordance with the principles of FIGS. 11-13 .
[0081] FIG. 26 is a functional exploded view of the heat transfer system of FIG. 25 .
[0082] FIG. 27 is a partial cross-sectional detail view of an evaporator used in the heat transfer system of FIG. 25 .
[0083] FIG. 28 is a perspective view of a heat exchanger used in the heat transfer system of FIG. 25 .
[0084] FIG. 29 is a graph of temperature of a heat source of a cyclical heat exchange system versus a surface area of an interface between the heat transfer system and the heat source of the cyclical heat exchange system.
[0085] FIG. 30 is a top plan view of a heat transfer system packaged around a portion of a cyclical heat exchange system.
[0086] FIG. 31 is a partial cross-sectional elevation view (taken along line 31-31) of the heat transfer system packaged around the cyclical heat exchange system portion of FIG. 30 .
[0087] FIG. 32 is a partial cross-sectional elevation view (taken at detail 3200) of the interface between the heat transfer system and the cyclical heat exchange system of FIG. 30 .
[0088] FIG. 33 is an upper perspective view of a heat transfer system mounted to a cyclical heat exchange system.
[0089] FIG. 34 is a lower perspective view of the heat transfer system mounted to the cyclical heat exchange system of FIG. 33 .
[0090] FIG. 35 is a partial cross-sectional view of an interface between an evaporator of a heat transfer system and a cyclical heat exchange system in which the evaporator is clamped onto the cyclical heat exchange system.
[0091] FIG. 36 is a side view of a clamp used to clamp the evaporator onto the cyclical heat exchange system of FIG. 35 .
[0092] FIG. 37 is a partial cross-sectional view of an interface between an evaporator of a heat transfer system and a cyclical heat exchange system in which the interface is formed by an interference fit between the evaporator and the cyclical heat exchange system.
[0093] FIG. 38 is a partial cross-sectional view of an interface between an evaporator of a heat transfer system and a cyclical heat exchange system in which the interface is formed by forming the evaporator integrally with the cyclical heat exchange system.
[0094] FIG. 39 is a top plan view of a condenser of a heat transfer system.
[0095] FIG. 40 is a partial cross-sectional view taken along line 40-40 of the condenser of FIG. 39 .
[0096] FIGS. 41-43 are detail cross-sectional views of a condenser having a laminated construction.
[0097] FIG. 44 is a detail cross-sectional view of a condenser having an extruded construction.
[0098] FIG. 45 is a perspective detail and cross-sectional view of a condenser having an extruded construction.
[0099] FIG. 46 is a cross-sectional view of one side of a heat transfer system packaging around a cyclical heat exchange system.
[0100] Like reference symbols in the various drawings indicate like elements.
Detailed Description
[0101] As discussed above, in a loop heat pipe (LHP), the reservoir is co-located with the evaporator, thus, the reservoir is thermally and hydraulically connected with the reservoir through a heat-pipe-like conduit. In this way, liquid from the reservoir can be pumped to the evaporator, thus ensuring that the primary wick of the evaporator is sufficiently wetted or “primed” during start-up. Additionally, the design of the LHP also reduces depletion of liquid from the primary wick of the evaporator during steady-state or transient operation of the evaporator within a heat transport system. Moreover, vapor and/or bubbles of non-condensable gas (NCG bubbles) vent from a core of the evaporator through the heat-pipe-like conduit into the reservoir.
[0102] Conventional LHPs require that liquid be present in the reservoir prior to start-up, that is, application of power to the evaporator of the LHP. However, if the working fluid in the LHP is in a supercritical state prior to start-up of the LHP, liquid will not be present in the reservoir prior to start-up. A supercritical state is a state in which a temperature of the LHP is above the critical temperature of the working fluid. The critical temperature of a fluid is the highest temperature at which the fluid can exhibit a liquid-vapor equilibrium. For example, the LHP may be in a supercritical state if the working fluid is a cryogenic fluid, that is, a fluid having a boiling point below −150° C., or if the working fluid is a sub-ambient fluid, that is, a fluid having a boiling point below the temperature of the environment in which the LHP is operating.
[0103] Conventional LHPs also require that liquid returning to the evaporator is subcooled, that is, cooled to a temperature that is lower than the boiling point of the working fluid. Such a constraint makes it impractical to operate LHPs at a sub-ambient temperature. For example, if the working fluid is a cryogenic fluid, the LHP is likely operating in an environment having a temperature greater than the boiling point of the fluid.
[0104] Referring to FIG. 1 , a heat transport system 100 is designed to overcome limitations of conventional LHPs. The heat transport system 100 includes a heat transfer system 105 and a priming system 110. The priming system 110 is configured to convert fluid within the heat transfer system 105 into a liquid, thus priming the heat transfer system 105. As used in this description, the term “fluid” is a generic term that refers to a substance that is both a liquid and a vapor in saturated equilibrium.
[0105] The heat transfer system 105 includes a main evaporator 115, and a condenser 120 coupled to the main evaporator 115 by a liquid line 125 and a vapor line 130. The condenser 120 is in thermal communication with a heat sink 165, and the main evaporator 115 is in thermal communication with a heat source Qin 116. The heat transfer system 105 may also include a hot reservoir 147 coupled to the vapor line 130 for additional pressure containment, as needed. In particular, the hot reservoir 147 increases the volume of the heat transport system 100. If the working fluid is at a temperature above its critical temperature, that is, the highest temperature at which the working fluid can exhibit liquid-vapor equilibrium, its pressure is proportional to the mass in the heat transport system 100 (the charge) and inversely proportional to the volume of the heat transport system 100. Increasing the volume with the hot reservoir 147 lowers the fill pressure.
[0106] The main evaporator 115 includes a container 117 that houses a primary wick 140 within which a core 135 is defined. The main evaporator 115 includes a bayonet tube 142 and a secondary wick 145 within the core 135. The bayonet tube 142, the primary wick 140, and the secondary wick 145 define a liquid passage 143, a first vapor passage 144, and a second vapor passage 146. The secondary wick 145 provides phase control, that is, liquid/vapor separation in the core 135, as discussed in U.S. patent application Ser. No. 09/896,561, filed Jun. 29, 2001, now U.S. Pat. No. 6,889,754, issued May 10, 2005, which is incorporated herein by reference in its entirety. As shown, the main evaporator 115 has three ports, a liquid inlet 137 into the liquid passage 143, a vapor outlet 132 into the vapor line 130 from the second vapor passage 146, and a fluid outlet 139 from the liquid passage 143 (and possibly the first vapor passage 144, as discussed below). Further details on the structure of a three-port evaporator are discussed below with respect to FIGS. 5A and 5B .
[0107] The priming system 110 includes a secondary or priming evaporator 150 coupled to the vapor line 130 and a reservoir 155 co-located with the secondary evaporator 150. The reservoir 155 is coupled to the core 135 of the main evaporator 115 by a secondary fluid line 160 and a secondary condenser 122. The secondary fluid line 160 couples to the fluid outlet 139 of the main evaporator 115. The priming system 110 also includes a controlled heat source Qsp 151 in thermal communication with the secondary evaporator 150.
[0108] The secondary evaporator 150 includes a container 152 that houses a primary wick 190 within which a core 185 is defined. The secondary evaporator 150 includes a bayonet tube 153 and a secondary wick 180 that extends from the core 185, through a conduit 175, and into the reservoir 155. The secondary wick 180 provides a capillary link between the reservoir 155 and the secondary evaporator 150. The bayonet tube 153, the primary wick 190, and the secondary wick 180 define a liquid passage 182 coupled to the secondary fluid line 160, a first vapor passage 181 coupled to the reservoir 155, and a second vapor passage 183 coupled to the vapor line 130. The reservoir 155 is thermally and hydraulically coupled to the core 185 of the secondary evaporator 150 through the liquid passage 182, the secondary wick 180, and the first vapor passage 181. Vapor and/or NCG bubbles from the core 185 of the secondary evaporator 150 are swept through the first vapor passage 181 to the reservoir 155 and condensable liquid is returned to the secondary evaporator 150 through the secondary wick 180 from the reservoir 155. The primary wick 190 hydraulically links liquid within the core 185 of the secondary evaporator 150 to the controlled heat source Qsp 151, permitting liquid at an outer surface of the primary wick 190 to evaporate and form vapor within the second vapor passage 183 when heat is applied to the secondary evaporator 150.
[0109] The reservoir 155 is cold-biased, and thus, it is cooled by a cooling source that will allow it to operate, if unheated, at a temperature that is lower than the temperature at which the heat transfer system 105 operates. In one implementation, the reservoir 155 and the secondary condenser 122 are in thermal communication with the heat sink 165 that is thermally coupled to the condenser 120. For example, the reservoir 155 can be mounted to the heat sink 165 using a shunt 170, which may be made of aluminum or any heat conductive material. In this way, the temperature of the reservoir 155 tracks the temperature of the condenser 120.
[0110] FIG. 2 shows an example of an implementation of the heat transport system 100. In this implementation, the condensers 120 and 122 are mounted to a cryocooler 200, which acts as a refrigerator, transferring heat from the condensers 120, 122 to the heat sink 165. Additionally, in the implementation of FIG. 2 , the lines 125, 130, 160 are wound to reduce space requirements for the heat transport system 100.
[0111] Though not shown in FIGS. 1 and 2 , elements such as, for example, the reservoir 155 and the main evaporator 115, may be equipped with temperature sensors that can be used for diagnostic or testing purposes.
[0112] Referring also to FIG. 3 , the heat transport system 100 performs a procedure 300 for transporting heat from the heat source Qin 116 and for ensuring that the main evaporator 115 is wetted with liquid prior to startup. The procedure 300 is particularly useful when the heat transfer system 105 is at a supercritical state. Prior to initiation of the procedure 300, the heat transport system 100 is filled with a working fluid at a particular pressure, referred to as a “fill pressure.”
[0113] Initially, the reservoir 155 is cold-biased by, for example, mounting the reservoir 155 to the heat sink 165 (step 305). The reservoir 155 may be cold-biased to a temperature below the critical temperature of the working fluid, which, as discussed, is the highest temperature at which the working fluid can exhibit liquid-vapor equilibrium. For example, if the fluid is ethane, which has a critical temperature of 33° C., the reservoir 155 is cooled to below 33° C. As the temperature of the reservoir 155 drops below the critical temperature of the working fluid, the reservoir 155 partially fills with a liquid condensate formed by the working fluid. The formation of liquid within the reservoir 155 wets the secondary wick 180 and the primary wick 190 of the secondary evaporator 150 (step 310).
[0114] Meanwhile, power is applied to the priming system 110 by applying heat from the heat source Qsp 151 to the secondary evaporator 150 (step 315) to enhance or initiate circulation of fluid within the heat transfer system 105. Vapor output by the secondary evaporator 150 is pumped through the vapor line 130 and through the condenser 120 (step 320) due to capillary pressure at the interface between the primary wick 190 and the second vapor passage 183. As vapor reaches the condenser 120, it is converted to liquid (step 325). The liquid formed in the condenser 120 is pumped to the main evaporator 115 of the heat transfer system 105 (step 330). When the main evaporator 115 is at a higher temperature than the critical temperature of the fluid, the liquid entering the main evaporator 115 evaporates and cools the main evaporator 115. This process (steps 315-330) continues, causing the main evaporator 115 to reach a set point temperature (step 335), at which point the main evaporator 115 is able to retain liquid and be wetted and to operate as a capillary pump. In one implementation, the set point temperature is the temperature to which the reservoir 155 has been cooled. In another implementation, the set point temperature is a temperature below the critical temperature of the working fluid. In a further implementation, the set point temperature is a temperature above the temperature to which the reservoir 155 has been cooled.
[0115] If the set point temperature has been reached (step 335), the heat transport system 100 operates in a main mode (step 340) in which heat from the heat source Qin 116 that is applied to the main evaporator 115 is transferred by the heat transfer system 105. Specifically, in the main mode, the main evaporator 115 develops capillary pumping to promote circulation of the working fluid through the heat transfer system 105. Also, in the main mode, the set point temperature of the reservoir 155 is reduced. The rate at which the heat transfer system 105 cools down during the main mode depends on the cold-biasing of the reservoir 155 because the temperature of the main evaporator 115 closely follows the temperature of the reservoir 155. Additionally, though not required, a heater can be used to further control or regulate the temperature of the reservoir 155 during the main mode (step 340). Furthermore, in the main mode, the power applied to the secondary evaporator 150 by the controlled heat source Qsp 151 is reduced, thus bringing the heat transfer system 105 down to a normal operating temperature for the fluid. For example, in the main mode, the heat load from the controlled heat source Qsp 151 to the secondary evaporator 150 is kept at a value equal to or in excess of heat conditions, as defined below. In one implementation, the heat load from the controlled heat source Qsp is kept to about 5 to 10% of the heat load applied to the main evaporator 115 from the heat source Qin 116.
[0116] In this particular implementation, the main mode is triggered by the determination that the set point temperature has been reached (step 335). In other implementations, the main mode may begin at other times or due to other triggers. For example, the main mode may begin after the priming system is wet (step 310) or after the reservoir has been cold biased (step 305).
[0117] At any time during operation, the heat transfer system 105 can experience heat conditions such as those resulting from heat conduction across the primary wick 140 and parasitic heat applied to the liquid line 125. Both conditions cause formation of vapor on the liquid side of the evaporator. Specifically, heat conduction across the primary wick 140 can cause liquid in the core 135 to form vapor bubbles, which, if left within the core 135, would grow and block off liquid supply to the primary wick 140, thus causing the main evaporator 115 to fail. Parasitic heat input into the liquid line 125 (referred to as “parasitic heat gains”) can cause liquid within the liquid line 125 to form vapor.
[0118] To reduce the adverse impact of heat conditions discussed above, the priming system 110 operates at a power level greater than or equal to the sum of the head conduction and the parasitic heat gains. As mentioned above, for example, the priming system 110 can operate at 5 to 10% of the power to the heat transfer system 105. In particular, fluid that includes a combination of vapor bubbles and liquid is swept out of the core 135 for discharge into the secondary fluid line 160 leading to the secondary condenser 122. In particular, vapor that forms within the core 135 travels around the bayonet tube 142 directly into the fluid outlet port 139. Vapor that forms within the first vapor passage 144 makes it way into the fluid outlet port 139 by either traveling through the secondary wick 145 (if the pore size of the secondary wick 145 is large enough to accommodate vapor bubbles) or through an opening at an end of the secondary wick 145 near the outlet port 139 that provides a clear passage from the first vapor passage 144 to the outlet port 139. The secondary condenser 122 condenses the bubbles in the fluid and pushes the fluid to the reservoir 155 for reintroduction into the heat transfer system 105.
[0119] Similarly, to reduce parasitic heat input to the liquid line 125, the secondary fluid line 160 and the liquid line 125 can form a coaxial configuration and the secondary fluid line 160 surrounds and insulates the liquid line 125 from surrounding heat. This implementation is discussed further below with reference to FIGS. 8A and 8B . As a consequence of this configuration, it is possible for the surrounding heat to cause vapor bubbles to form in the secondary fluid line 160, instead of in the liquid line 125. As discussed, by virtue of capillary action effected at the secondary wick 145, fluid flows from the main evaporator 115 to the secondary condenser 122. This fluid flow, and the relatively low temperature of the secondary condenser 122, causes a sweeping of the vapor bubbles within the secondary fluid line 160 through the secondary condenser 122, where they are condensed into liquid and pumped into the reservoir 155.
[0120] As shown in FIG. 4 , data from a test run is shown. In this implementation, prior to startup of the main evaporator 115 at time 410, a temperature 400 of the main evaporator 115 is significantly higher than a temperature 405 of the reservoir 155, which has been cold-biased to the set point temperature (step 305). As the priming system 110 is wetted (step 310), power Qsp 450 is applied to the secondary evaporator 150 (step 315) at a time 452, causing liquid to be pumped to the main evaporator 115 (step 330), the temperature 400 of the main evaporator 115 drops until it reaches the temperature 405 of the reservoir 155 at time 410. Power Qin 460 is applied to the main evaporator 115 at a time 462, when the system 100 is operating in LHP mode (step 340). As shown, power input Qin 460 to the main evaporator 115 is held relatively low while the main evaporator 115 is cooling down. Also shown are the temperatures 470 and 475, respectively, of the secondary fluid line 160 and the liquid line 125. After time 410, temperatures 470 and 475 track the temperature 400 of the main evaporator 115. Moreover, a temperature 415 of the secondary evaporator 150 follows closely with the temperature 405 of the reservoir 155 because of the thermal communication between the secondary evaporator 150 and the reservoir 155.
[0121] As mentioned, in one implementation, ethane may be used as the fluid in the heat transfer system 105. Although the critical temperature of ethane is 33° C., for the reasons generally described above, the heat transport system 100 can start up from a supercritical state in which the heat transport system 100 is at a temperature of 70° C. As power Qsp 450 is applied to the secondary evaporator 150, the temperatures of the condenser 120 and the reservoir 155 drop rapidly (between times 452 and 410). A trim heater can be used to control the temperature of the reservoir 155 and thus the condenser 120 operates at a temperature of −10° C. To startup the main evaporator 115 from the supercritical temperature of 70° C., a heat load or power input Qsp of 10 W is applied to the secondary evaporator 150. Once the main evaporator 115 is primed, the power input from the controlled heat source Qsp 151 to the secondary evaporator 150 and the power applied to and through the trim heater both may be reduced to bring the temperature of the heat transport system 100 down to a nominal operating temperature of about −50° C. For instance, during the main mode, if a power input Qin of 40 W is applied to the main evaporator 115, the power input Qsp to the secondary evaporator 150 can be reduced to approximately 3 W while operating at −45° C. to mitigate the 3 W lost through heat conditions (as discussed above). As another example, the main evaporator 115 can operate with power input Qin from about 10 W to about 40 W with 5 W applied to the secondary evaporator 150 and with the temperature 405 of the reservoir 155 at approximately −45° C.
[0122] Referring to FIGS. 5A and 5B , in one implementation, the main evaporator 115 is designed as a three-port evaporator 500 (which is the design shown in FIG. 1 ). Generally, in the three-port evaporator 500, liquid flows into a liquid inlet 505 and into a core 510, defined by a primary wick 540, and fluid from the core 510 flows from a fluid outlet 512 to a cold-biased reservoir (such as reservoir 155). The fluid and the core 510 are housed within a container 515 made of, for example, aluminum. In particular, fluid flowing from the liquid inlet 505 into the core 510 flows through a bayonet tube 520, into a liquid passage 521 that flows through and around the bayonet tube 520. Fluid can flow through a secondary wick 525 (such as secondary wick 145 of main evaporator 115) made of a wick material 530 and an annular artery 535. The wick material 530 separates the annular artery 535 from a first vapor passage 560. As power from the heat source Qin 116 is applied to the evaporator 500, liquid from the core 510 enters a primary wick 540 and evaporates, forming vapor that is free to flow along a second vapor passage 565 that includes one or more vapor grooves 545 and out a vapor outlet 550 into the vapor line 130. Vapor bubbles that form within first vapor passage 560 of the core 510 are swept out of the core 510 through the first vapor passage 560 and into the fluid outlet 512. As discussed above, vapor bubbles within the first vapor passage 560 may pass through the secondary wick 525 if the pore size of the secondary wick 525 is large enough to accommodate the vapor bubbles. Alternatively, or additionally, vapor bubbles within the first vapor passage 560 may pass through an opening of the secondary wick 525 formed at any suitable location along the secondary wick 525 to enter the liquid passage 521 or the fluid outlet 512.
[0123] Referring to FIG. 6 , in another implementation, the main evaporator 115 is designed as a four-port evaporator 600, which is a design described in U.S. patent application Ser. No. 09/896,561, filed Jun. 29, 2001, now U.S. Pat. No. 6,889,754, issued May 10, 2005. Briefly, and with emphasis on aspects that differ from the three-port evaporator configuration, liquid flows into the evaporator 600 through a fluid inlet 605, through a bayonet tube 610, and into a core 615. The liquid within the core 615 enters a primary wick 620 and evaporates, forming vapor that is free to flow along vapor grooves 625 and out a vapor outlet 630 into the vapor line 130. A secondary wick 633 within the core 615 separates liquid within the core from vapor or bubbles in the core (that are produced when liquid in the core 615 heats). The liquid carrying bubbles formed within a first fluid passage 635 inside the secondary wick 633 flows out of a fluid outlet 640 and the vapor or bubbles formed within a vapor passage 642 positioned between the secondary wick 633 and the primary wick 620 flow out of a vapor outlet 645.
[0124] Referring also to FIG. 7 , a heat transport system 700 is shown in which the main evaporator is a four-port evaporator 600. The heat transport system 700 includes one or more heat transfer systems 705 and a priming system 710 configured to convert fluid within the heat transfer systems 705 into a liquid to prime the heat transfer systems 705. The four-port evaporators 600 are coupled to one or more condensers 715 by a vapor line 720 and a fluid line 725. The priming system 710 includes a cold-biased reservoir 730 hydraulically and thermally connected to a priming evaporator 735.
[0125] Design considerations of the heat transport system 100 include startup of the main evaporator 115 from a supercritical state, management of parasitic heat leaks, heat conduction across the primary wick 140, cold-biasing of the cold reservoir 155, and pressure containment at ambient temperatures that are greater than the critical temperature of the working fluid within the heat transfer system 105. To accommodate these design considerations, the body or container (such as container 515) of the main evaporator 115 or secondary evaporator 150 can be made of extruded 6063 aluminum and the primary wicks 140 and/or 190 can be made of a fine-pored wick. In one implementation, the outer diameter of the main evaporator 115 or secondary evaporator 150 is approximately 0.625 inch and the length of the container is approximately 6 inches. The reservoir 155 may be cold-biased to an end panel of the heat sink 165 using the aluminum shunt 170. Furthermore, a heater (such as KAPTON® heater) can be attached at a side of the reservoir 155.
[0126] In one implementation, the vapor line 130 is made with smooth walled stainless steel tubing having an outer diameter (OD) of 3/16″ and the liquid line 125 and the secondary fluid line 160 are made of smooth walled stainless steel tubing having an OD of ⅛″. The lines 125, 130, 160 may be bent in a serpentine route and plated with gold to minimize parasitic heat gains. Additionally, the lines 125, 130, 160 may be enclosed in a stainless steel box with heaters to simulate a particular environment during testing. The stainless steel box can be insulated with multi-layer insulation (MLI) to minimize heat leaks through panels of the heat sink 165.
[0127] In one implementation, the secondary condenser 122 and the secondary fluid line 160 are made of tubing having an OD of 0.25 inch. The tubing is bonded to the panels of the heat sink 165 using, for example, epoxy. Each panel of the heat sink 165 is an 8×19-inch direct condensation, aluminum radiator that uses a 1/16-inch thick face sheet. KAPTON® heaters can be attached to the panels of the heat sink 165, near the condenser 120 to prevent inadvertent freezing of the working fluid. During operation, temperature sensors such as thermocouples can be used to monitor temperatures throughout the heat transport system 100.
[0128] The heat transport system 100 may be implemented in any circumstances where the critical temperature of the working fluid of the heat transfer system 105 is below the ambient temperature at which the heat transport system 100 is operating. The heat transport system 100 can be used to cool down components that require cryogenic cooling.
[0129] Referring to FIGS. 8A-8D , the heat transport system 100 may be implemented in a miniaturized cryogenic system 800. In the miniaturized system 800, the lines 125, 130, 160 are made of flexible material to permit coil configurations 805, which save space. The miniaturized system 800 can operate at −238° C. using neon fluid. Power input Qin 116 is approximately 0.3 to 2.5 W. The miniaturized system 800 thermally couples a cryogenic component (or heat source that requires cryogenic cooling) 816 to a cryogenic cooling source such as a cryocooler 810 coupled to cool the condensers 120, 122.
[0130] The miniaturized system 800 reduces mass, increases flexibility, and provides thermal switching capability when compared with traditional thermally switchable vibration-isolated systems. Traditional thermally switchable vibration-isolated systems require two flexible conductive links (FCLs), a cryogenic thermal switch (CTSW), and a conduction bar (CB) that form a loop to transfer heat from the cryogenic component to the cryogenic cooling source. In the miniaturized system 800, thermal performance is enhanced because the number of mechanical interfaces is reduced. Heat conditions at mechanical interfaces account for a large percentage of heat gains within traditional thermally switchable vibration-isolated systems. The CB and two FCLs are replaced with the low-mass, flexible, thin-walled tubing used for the coil configurations 805 of the miniaturized system 800.
[0131] Moreover, the miniaturized system 800 can function in a wide range of heat transport distances, which permits a configuration in which the cooling source (such as the cryocooler 810) is located remotely from the cryogenic component 816. The coil configurations 805 have a low mass and low surface area, thus reducing parasitic heat gains through the lines 125 and 160. The configuration of the cooling source 810 within the miniaturized system 800 facilitates integration and packaging of the miniaturized system 800 and reduces vibrations on the cooling source 810, which becomes particularly important in infrared sensor applications. In one implementation, the miniaturized system 800 was tested using neon, operating at 25 to 40K.
[0132] Referring to FIGS. 9A-9C , the heat transport system 100 may be implemented in an adjustable mounted or gimbaled system 1005 in which the main evaporator 115 and a portion of the lines 125, 160, and 130 are mounted to rotate about an elevation axis within a range of ±45° and a portion of the lines 125, 160, and 130 are mounted to rotate about an azimuth axis within a range of ±220°. The lines 125, 160, 130 are formed from thin-walled tubing and are coiled around each axis of rotation. The system 1005 thermally couples a cryogenic component (or heat source that requires cryogenic cooling) such as a sensor 1016 of a cryogenic telescope to a cryogenic cooling source 1010 such as a cryocooler coupled to cool the condensers 120, 122. The cooling source 1010 is located at a stationary spacecraft 1060, thus reducing mass at the cryogenic telescope. Motor torque for controlling rotation of the lines 125, 160, 130, power requirements of the system 1005, control requirements for the spacecraft 1060, and pointing accuracy for the sensor 1016 are improved. The cooling source 1010 and the radiator or heat sink 165 can be moved from the sensor 1016, reducing vibration within the sensor 1016. In one implementation, the system 1005 was tested to operate within the range of 70 to 115 K when the working fluid is nitrogen.
[0133] The heat transfer system 105 may be used in medical applications, or in applications where equipment must be cooled to below-ambient temperatures. As another example, the heat transfer system 105 may be used to cool an infrared (IR) sensor that operates at cryogenic temperatures to reduce ambient noise. The heat transfer system 105 may be used to cool a vending machine, which often houses items that preferably are chilled to sub-ambient temperatures. The heat transfer system 105 may be used to cool components such as a display or a hard drive of a computer, such as a laptop computer, handheld computer, or a desktop computer. The heat transfer system 105 can be used to cool one or more components in a transportation device such as an automobile or an airplane.
[0134] Other implementations are within the scope of the following claims. For example, the condenser 120 and heat sink 165 can be designed as an integral system, such as, a radiator. Similarly, the secondary condenser 122 and heat sink 165 can be formed from a radiator. The heat sink 165 can be a passive heat sink (such as a radiator) or a cryocooler that actively cools the condensers 120, 122.
[0135] In another implementation, the temperature of the reservoir 155 is controlled using a heater. In a further implementation, the reservoir 155 is heated using parasitic heat.
[0136] In another implementation, a coaxial ring of insulation is formed and placed between the liquid line 125 and the secondary fluid line 160, which surrounds the insulation ring.
[0137] Evaporator Design
[0138] Evaporators are integral components in two-phase heat transfer systems. For example, as shown above in FIGS. 5A and 5B , the evaporator 500 includes an evaporator body or container 515 that is in contact with the primary wick 540 that surrounds the core 510. The core 510 defines a flow passage for the working fluid. The primary wick 540 is surrounded at its periphery by a plurality of peripheral flow channels or vapor grooves 545. The channels 545 collect vapor at the interface between the wick 540 and the evaporator body 515. The channels 545 are in contact with the vapor outlet 550 that feeds into the vapor line 130 that feeds into the condenser to enable evacuation of the vapor formed within the main evaporator 115.
[0139] The evaporator 500 and the other evaporators discussed above often have a cylindrical geometry, that is, the core of the evaporator forms a cylindrical passage through which the working fluid passes. The cylindrical geometry of the evaporator is useful for cooling applications in which the heat acquisition surface is cylindrically hollow. Many cooling applications require that heat be transferred away from a heat source having a flat surface. In these sort of applications, the evaporator can be modified to include a flat conductive saddle to match the footprint of the heat source having the flat surface. Such a design is shown, for example, in U.S. Pat. No. 6,382,309.
[0140] The cylindrical geometry of the evaporator facilitates compliance with thermodynamic constraints of LHP operation (that is, the minimization of heat leaks into the reservoir). The constraints of LHP operation stem from the amount of subcooling an LHP needs to produce for normal equilibrium operation. Additionally, the cylindrical geometry of the evaporator is relatively easy to fabricate, handle, machine, and process.
[0141] However, as will be described hereinafter, an evaporator can be designed with a planar form to more naturally attach to a flat heat source.
[0142] Planar Design
[0143] Referring to FIG. 10 , an evaporator 1000 for a heat transfer system includes a heated wall 1005, a liquid barrier wall 1011, a primary wick 1015 between the heated wall 1005 and the inner side of the liquid barrier wall 1011, vapor removal channels 1020, and liquid flow channels 1025.
[0144] The heated wall 1005 is in intimate contact with the primary wick 1015. The liquid barrier wall 1011 contains working fluid on an inner side of the liquid barrier wall 1011 such that the working fluid flows only along the inner side of the liquid barrier wall 1011. The liquid barrier wall 1011 closes the evaporator's envelope and helps to organize and distribute the working fluid through the liquid flow channels 1025. The vapor removal channels 1020 are located at an interface between a vaporization surface 1017 of the primary wick 1015 and the heated wall 1005. The liquid flow channels 1025 are located between the liquid barrier wall 1011 and the primary wick 1015.
[0145] The heated wall 1005 acts as a heat acquisition surface for a heat source. The heated wall 1005 is made from a heat-conductive material, such as, for example, sheet metal. Material chosen for the heated wall 1005 typically is able to withstand internal pressure of the working fluid.
[0146] The vapor removal channels 1020 are designed to balance the hydraulic resistance of the vapor removal channels 1020 with the heat conduction through the heated wall 1005 into the primary wick 1015. The vapor removal channels 1020 can be electro-etched, machined, or formed in a surface with any other convenient method.
[0147] The vapor removal channels 1020 are shown as grooves in the inner side of the heated wall 1005. However, the vapor removal channels 1020 can be designed and located in several different ways, depending on the design approach chosen. For example, according to other implementations, the vapor removal channels 1020 are grooved into an outer surface of the primary wick 1015 or embedded into the primary wick 1015 such that they are under the surface of the primary wick 1015. The design of the vapor removal channels 1020 is selected to increase the ease and convenience of manufacturing and to closely approximate one or more of the following guidelines.
[0148] First, the hydraulic diameter of the vapor removal channels 1020 should be sufficient to handle a vapor flow generated on the vaporization surface 1017 of the primary wick 1015 without a significant pressure drop. Second, the surface of contact between the heated wall 1005 and the primary wick 1015 should be maximized to provide efficient heat transfer from the heat source to vaporization surface 1017 of the primary wick 1015. Third, a thickness 1030 of the heated wall 1005, which is in contact with the primary wick 1015, should be minimized. As the thickness 1030 increases, vaporization at the surface of the primary wick 1015 is reduced and transport of vapor through the vapor removal channels 1020 is reduced.
[0149] The evaporator 1000 can be assembled from separate parts. Alternatively, the evaporator 1000 can be made as a single part by in-situ sintering of the primary wick 1015 between two walls having special mandrels to form channels on both sides of the primary wick 1015.
[0150] The primary wick 1015 provides the vaporization surface 1017 and pumps or feeds the working fluid from the liquid flow channels 1025 to the vaporization surface 1017 of the primary wick 1015.
[0151] The size and design of the primary wick 1015 involves several considerations. The thermal conductivity of the primary wick 1015 should be low enough to reduce heat leak from the vaporization surface 1017, through the primary wick 1015, and to the liquid flow channels 1025. Heat leakage can also be affected by the linear dimensions of the primary wick 1015. For this reason, the linear dimensions of the primary wick 1015 should be properly optimized to reduce heat leakage. For example, an increase in a thickness 1019 of the primary wick 1015 can reduce heat leakage. However, increased thickness 1019 can increase hydraulic resistance of the primary wick 1015 to the flow of the working fluid. In working LHP designs, hydraulic resistance of the working fluid due to the primary wick 1015 can be significant and a proper balancing of these factors is important.
[0152] The force that drives or pumps the working fluid of a heat transfer system is a temperature or pressure difference between vapor and liquid sides of a primary wick. The pressure difference is supported by the primary wick and it is maintained by proper management of the incoming working fluid thermal balance.
[0153] The liquid returning to the evaporator from the condenser passes through a liquid return line and is slightly subcooled. The degree of subcooling offsets the heat leak through the primary wick and the heat leak from the ambient into the reservoir within the liquid return line. The subcooling of the liquid maintains a thermal balance of the reservoir. However, there exist other useful methods to maintain thermal balance of the reservoir.
[0154] One method is an organized heat exchange between reservoir and the environment. For evaporators having a planar design, such as those often used for terrestrial applications, the heat transfer system includes heat exchange fins on the reservoir and/or on the liquid barrier wall 1011 of the evaporator 1000. The forces of natural convection on these fins provide subcooling and reduce stress on the condenser and the reservoir of the heat transfer system.
[0155] The temperature of the reservoir or the temperature difference between the reservoir and the vaporization surface 1017 of the primary wick 1015 supports the circulation of the working fluid through the heat transfer system. Some heat transfer systems may require an additional amount of subcooling. The required amount may be greater than what the condenser can produce, even if the condenser is completely blocked.
[0156] In designing the evaporator 1000, three variables need to be managed. First, the organization and design of the liquid flow channels 1025 needs to be determined. Second, the venting of the vapor from the liquid flow channels 1025 needs to be accounted for. Third, the evaporator 1000 should be designed to ensure that liquid fills the liquid flow channels 1025. These three variables are interrelated and thus should be considered and optimized together to form an effective heat transfer system.
[0157] As mentioned, it is important to obtain a proper balance between the heat leak into the liquid side of the evaporator and the pumping capabilities of the primary wick. This balancing process cannot be done independently from the optimization of the condenser, which provides subcooling, because the greater heat leak allowed in the design of the evaporator, the more subcooling needs to be produced in the condenser. The longer the condenser, the greater are the hydraulic losses in a fluid line, which may require different wick material with better pumping capabilities.
[0158] In operation, as power from a heat source is applied to the evaporator 1000, liquid from the liquid flow channels 1025 enters the primary wick 1015 and evaporates, forming vapor that is free to flow along the vapor removal channels 1020. Liquid flow into the evaporator 1000 is provided by the liquid flow channels 1025. The liquid flow channels 1025 supply the primary wick 1015 with enough liquid to replace liquid that is vaporized on the vapor side of the primary wick 1015 and to replace liquid that is vaporized on the liquid side of the primary wick 1015.
[0159] The evaporator 1000 may include a secondary wick 1040, which provides phase management on a liquid side of the evaporator 1000 and supports feeding of the primary wick 1015 in critical modes of operation (as discussed above). The secondary wick 1040 is formed between the liquid flow channels 1025 and the primary wick 1015. The secondary wick 1040 can be a mesh screen (as shown in the FIG. 10 ), or an advanced and complicated artery, or a slab wick structure. Additionally, the evaporator 1000 may include a vapor vent channel 1045 at an interface between the primary wick 1015 and the secondary wick 1040.
[0160] Heat conduction through the primary wick 1015 may initiate vaporization of the working fluid in a wrong place, on a liquid side of the evaporator 1000 near or within the liquid flow channels 1025. The vapor vent channel 1045 delivers the unwanted vapor away from the primary wick 1015 into the two-phase reservoir.
[0161] The fine pore structure of the primary wick 1015 can create a significant flow resistance for the liquid. Therefore, it is important to optimize the number, the geometry, and the design of the liquid flow channels 1025. The goal of this optimization is to support a uniform, or close to uniform, feeding flow to the vaporization surface 1017. Moreover, as the thickness 1019 of the primary wick 1015 is reduced, the liquid flow channels 1025 can be spaced farther apart.
[0162] The evaporator 1000 may require significant vapor pressure to operate with a particular working fluid within the evaporator 1000. Use of a working fluid with a high vapor pressure can cause several problems with pressure containment of the evaporator envelope. Traditional solutions to the pressure containment problem, such as thickening the walls of the evaporator, are not always effective. For example, in planar evaporators having a significant flat area, the walls become so thick that the temperature difference is increased and the evaporator heat conductance is degraded. Additionally, even microscopic deflection of the walls due to the pressure containment results in a loss of contact between the walls and the primary wick. Such a loss of contact impacts heat transfer through the evaporator. And, microscopic deflection of the walls creates difficulties with the interfaces between the evaporator and the heat source and any external cooling equipment.
[0163] Annular Design
[0164] Referring to FIGS. 11-13 , an annular evaporator 1100 is formed by effectively rolling the planar evaporator 1000 such that the primary wick 1015 loops back into itself and forms an annular shape. The evaporator 1100 can be used in applications in which the heat sources have a cylindrical exterior profile, or in applications where the heat source can be shaped as a cylinder. The annular shape combines the strength of a cylinder for pressure containment and the curved interface surface for best possible contact with the cylindrically shaped heat sources.
[0165] The evaporator 1100 includes a heated wall 1105, a liquid barrier wall 1110, a primary wick 1115 positioned between the heated wall 1105 and the inner side of the liquid barrier wall 1110, vapor removal channels 1120, and liquid flow channels 1125. The liquid barrier wall 1110 is coaxial with the primary wick 1115 and the heated wall 1105.
[0166] The heated wall 1105 intimately contacts the primary wick 1115. The liquid barrier wall 1110 contains working fluid on an inner side of the liquid barrier wall 1110 such that the working fluid flows only along the inner side of the liquid barrier wall 1110. The liquid barrier wall 1110 closes the evaporator's envelope and helps to organize and distribute the working fluid through the liquid flow channels 1125.
[0167] The vapor removal channels 1120 are located at an interface between a vaporization surface 1117 of the primary wick 1115 and the heated wall 1105. The liquid flow channels 1125 are located between the liquid barrier wall 1110 and the primary wick 1115. The heated wall 1105 acts a heat acquisition surface and the vapor generated on this surface is removed by the vapor removal channels 1120.
[0168] The primary wick 1115 fills the volume between the heated wall 1105 and the liquid barrier wall 1110 of the evaporator 1100 to provide reliable reverse menisci vaporization.
[0169] The evaporator 1100 can also be equipped with heat exchange fins 1150 that contact the liquid barrier wall 1110 to cold bias the liquid barrier wall 1110. The liquid flow channels 1125 receive liquid from a liquid inlet 1155 and the vapor removal channels 1120 extend to and provide vapor to a vapor outlet 1160.
[0170] The evaporator 1100 can be used in a heat transfer system that includes an annular reservoir 1165 adjacent the primary wick 1115. The reservoir 1165 may be cold biased with the heat exchange fins 1150, which extend across the reservoir 1165. The cold biasing of the reservoir 1165 permits utilization of the entire condenser area without the need to generate subcooling at the condenser. The excessive cooling provided by cold biasing the reservoir 1165 and the evaporator 1100 compensates the parasitic heat leaks through the primary wick 1115 into the liquid side of the evaporator 1100.
[0171] In another implementation, the evaporator design can be inverted and vaporization features can be placed on an outer perimeter and the liquid return features can be placed on the inner perimeter.
[0172] The annular shape of the evaporator 1100 may provide one or more of the following or additional advantages. First, problems with pressure containment may be reduced or eliminated in the annular evaporator 1100. Second, the primary wick 1115 may not need to be sintered inside, thus providing more space for a more sophisticated design of the vapor and liquid sides of the primary wick 1115.
[0173] Referring also to FIGS. 14A-14H , an annular evaporator 1400 is shown having a liquid inlet 1455 and a vapor outlet 1460. The annular evaporator 1400 includes a heated wall 1700 (FIGS. 14G , 14H, 15A, and 15B), a liquid barrier wall 1500 (FIGS. 14G , 14H, and 17A-17D), a primary wick 1600 (FIGS. 14G , 14H, and 16A-16D) positioned between the heated wall 1700 and the inner side of the liquid barrier wall 1500, vapor removal channels 1465 (FIGS. 14H , 15A, and 15B), and liquid flow channels 1505 (FIGS. 14H ). The annular evaporator 1400 also includes a ring 1800 (FIGS. 14G and 18A-18D) that ensures spacing between the heated wall 1700 and the liquid barrier wall 1500 and a ring 1900 (FIGS. 14G , 14H, and 19A-19D) at a base of the evaporator 1400 that provides support for the liquid barrier wall 1500 and the primary wick 1600. The heated wall 1700, the liquid barrier wall 1500, the ring 1800, the ring 1900, and the primary wick 1600 are preferably formed of stainless steel.
[0174] The upper portion of the evaporator 1400 (that is, above the primary wick 1600) includes an expansion volume 1470 (FIG. 14H ). The liquid flow channels 1505, which are formed in the liquid barrier wall 1500, are fed by the liquid inlet 1455. The primary wick 1600 separates the liquid flow channels 1505 from the vapor removal channels 1465 that lead to the vapor outlet 1460 through a vapor annulus 1475 (FIG. 14H ) formed in the ring 1900. The vapor removal channels 1465 may be photo-etched into the surface of the heated wall 1700.
[0175] The evaporators disclosed herein can operate in any combination of materials, dimensions and arrangements, so long as they embody the features as described above. There are no restrictions other than criteria mentioned here; the evaporator can be made of any shape size and material. The only design constraints are that the applicable materials be compatible with each other and that the working fluid be selected in consideration of structural constraints, corrosion, generation of noncondensable gases, and lifetime issues.
[0176] Many terrestrial applications can incorporate an LHP with an annular evaporator 1100. The orientation of the annular evaporator in a gravity field is predetermined by the nature of application and the shape of the hot surface.
[0177] Cyclical Heat Exchange System
[0178] Cyclical heat exchange systems may be configured with one or more heat transfer systems to control a temperature at a region of the heat exchange system. The cyclical heat exchange system may be any system that operates using a thermodynamic cycle, such as, for example, a cyclical heat exchange system, a Stirling heat exchange system (also known as a Stirling engine), or an air conditioning system.
[0179] Referring to FIG. 20 , a Stirling heat exchange system 2000 utilizes a known type of environmentally friendly and efficient refrigeration cycle. The Stirling system 2000 functions by directing a working fluid (for example, helium) through four repetitive operations; that is, a heat addition operation at constant temperature, a constant volume heat rejection operation, a constant temperature heat rejection operation and a heat addition operation at constant volume.
[0180] The Stirling system 2000 is designed as a Free Piston Stirling Cooler (FPSC), such as Global Cooling's model M100B (Available from Global Cooling Manufacturing, 94 N. Columbus Rd., Athens, Ohio). The FPSC 2000 includes a linear motor portion 2005 housing a linear motor (not shown) that receives an AC power input 2010. The FPSC 2000 includes a heat acceptor 2015, a regenerator 2020, and a heat rejecter 2025. The FPSC 2000 includes a balance mass 2030 coupled to the body of the linear motor within the linear motor portion 2005 to absorb vibrations during operation of the FPSC 2000. The FPSC 2000 also includes a charge port 2035. The FPSC 2000 includes internal components, such as those shown in the FPSC 2100 of FIG. 21 .
[0181] The FPSC 2100 includes a linear motor 2105 housed within the linear motor portion 2110. The linear motor portion 2110 houses a piston 2115 that is coupled to flat springs 2120 at one end and a displacer 2125 at another end. The displacer 2125 couples to an expansion space 2130 and a compression space 2135 that form, respectively, cold and hot sides. The heat acceptor 2015 is mounted to the cold side of the expansion space 2130 and the heat rejector is mounted to the hot side of the compression space 2135. The FPSC 2100 also includes a balance mass 2140 coupled to the linear motor portion 2110 to absorb vibrations during operation of the FPSC 2100.
[0182] Referring also to FIG. 22 , in one implementation, a FPSC 2200 includes heat rejector 2205 made of a copper sleeve and a heat acceptor 2210 made of a copper sleeve. The heat rejector 2205 has an outer diameter (OD) of approximately 100 mm and a width of approximately 53 mm to provide a 166 cm2 heat rejection surface capable of providing a flux of −6 W/cm2 when operating in a temperature range of 20° C. to 70° C. The heat acceptor 2210 has an OD of approximately 100 mm and a width of approximately 37 mm to provide a 115 cm2 heat accepting surface capable of providing a flux of −5.2 W/cm2 in a temperature range of −30° C. to 5° C.
[0183] Briefly, in operation an FPSC is filled with a coolant (such as, for example, helium gas) that is shuttled back and forth by combined movements of the piston and the displacer. In an ideal system, thermal energy is rejected to the environment through the heat rejector while the coolant is compressed by the piston and thermal energy is extracted from the environment through the heat acceptor while the coolant expands.
[0184] Referring to FIG. 23 , a thermodynamic system 2300 includes a cyclical heat exchange system such as a cyclical heat exchange system 2305 (for example, the systems 2000, 2100, 2200) and a heat transfer system 2310 thermally coupled to a portion 2315 of the cyclical heat exchange system 2305. The cyclical heat exchange system 2305 is cylindrical and the heat transfer system 2310 is shaped to surround the portion 2315 of the cyclical heat exchange system 2305 to reject heat from the portion 2315. In this implementation, the portion 2315 is the hot side (that is, the heat rejector) of the cyclical heat exchange system 2305. The thermodynamic system 2300 also includes a fan 2320 positioned at the hot side of the cyclical heat exchange system 2305 to force air over a condenser of the heat transfer system 2310 and thus to provide additional convection cooling.
[0185] A cold side 2335 (that is, the heat acceptor) of the cyclical heat exchange system 2305 is thermally coupled to a CO2 refluxer 2340 of a thermosyphon 2345. The thermosyphon 2345 includes a cold-side heat exchanger 2350 that is configured to cool air within the thermodynamic system 2300 that is forced across the heat exchanger 2350 by a fan 2355.
[0186] Referring to FIG. 24 , in another implementation, a thermodynamic system 2400 includes a cyclical heat exchange system such as a cyclical heat exchange system 2405 (for example, the systems 2000, 2100, 2200) and a heat transfer system 2410 thermally coupled to a hot side 2415 of the cyclical heat exchange system 2405. The thermodynamic system 2400 includes a heat transfer system 2420 thermally coupled to a cold side 2425 of the cyclical heat exchange system 2405. The thermodynamic system 2400 also includes fans 2430, 2435. The fan 2430 is positioned at the hot side 2415 of the thermodynamic system to force air through a condenser of the heat transfer system 2410. The fan 2435 is positioned at the cold side 2425 of the thermodynamic system 2400 to force air through a condenser of the heat transfer system 2420.
[0187] Referring to FIG. 25 , in one implementation, a thermodynamic system 2500 includes a heat transfer system 2505 coupled to a cyclical heat exchange system such as a cyclical heat exchange system 2510. The heat transfer system 2505 is used to cool a hot side 2515 of the cyclical heat exchange system 2510. The heat transfer system 2505 includes an annular evaporator 2520 that includes an expansion volume (or reservoir) 2525, a liquid return line 2530 providing fluid communication between liquid outlets 2535 of a condenser 2540 and a liquid inlet of the evaporator 2520. The heat transfer system 2505 also includes a vapor line 2545 providing fluid communication between a vapor outlet of the evaporator 2520 and vapor inlets 2550 of the condenser 2540.
[0188] The condenser 2540 is constructed from smooth-wall tubing and is equipped with heat exchange fins 2555 or fin stock to intensify heat exchange on the outside of the tubing.
[0189] The evaporator 2520 includes a primary wick 2560 sandwiched between a heated wall 2565 and a liquid barrier wall 2570 and separating the liquid and the vapor. The liquid barrier wall 2570 is cold-biased by heat exchange fins 2575 formed along the outer surface of the heated wall 2565. The heat exchange fins 2575 provide subcooling for the reservoir 2525 and the entire liquid side of the evaporator 2520. The heat exchange fins 2575 of the evaporator 2520 may be designed separately from the heat exchange fins 2555 of the condenser 2540.
[0190] The liquid return line 2530 extends into the reservoir 2525 located above the primary wick 2560, and vapor bubbles, if any, from the liquid return line 2530 and the vapor removal channels at the interface of the primary wick 2560 and the heated wall 2565 are vented into the reservoir 2525. Typical working fluids for the heat transfer system 2505 include (but are not limited to) methanol, butane, CO2, propylene, and ammonia.
[0191] The evaporator 2520 is attached to the hot side 2515 of the cyclical heat exchange system 2510. In one implementation, this attachment is integral in that the evaporator 2520 is an integral part of the cyclical heat exchange system 2510. In another implementation, attachment can be non-integral in that the evaporator 2520 can be clamped to an outer surface of the hot side 2510. The heat transfer system 2505 is cooled by a forced convection sink, which can be provided by a simple fan 2580. Alternatively, the heat transfer system 2505 is cooled by a natural or draft convection.
[0192] Initially, the liquid phase of the working fluid is collected in a lower part of the evaporator 2520, the liquid return line 2530, and the condenser 2540. The primary wick 2560 is wet because of capillary forces. As soon as heat is applied (for example, the cyclical heat exchange system 2510 is turned on), the primary wick 2560 begins to generate vapor, which travels through vapor removal channels (similar to vapor removal channels 1120 of evaporator 1100) of the evaporator 2520, through the vapor outlet of the evaporator 2520, and into the vapor line 2545.
[0193] The vapor then enters the condenser 2540 at an upper part of the condenser 2540. The condenser 2540 condenses the vapor into liquid and the liquid is collected at a lower part of the condenser 2540. The liquid is pushed into the reservoir 2525 because of the pressure difference between the reservoir 2525 and the lower part of the condenser 2540. Liquid from the reservoir 2525 enters liquid flow channels of the evaporator 2520. The liquid flow channels of the evaporator 2520 are configured like the vapor removal channels 1125 of the evaporator 1100 and are properly sized and located to provide adequate liquid replacement for the liquid that vaporized. Capillary pressure created by the primary wick 2560 is sufficient to withstand the overall LHP pressure drop and to prevent vapor bubbles from travelling through the primary wick 2560 toward the liquid flow channels.
[0194] The liquid flow channels of the evaporator 2520 can be replaced by a simple annulus, if the cold biasing discussed above is sufficient to compensate the increased heat leak across the primary wick 2560, which is caused by the increase in surface area of the heat exchange surface of annulus versus the surface area of the liquid flow channels.
[0195] Referring to FIGS. 26-28 , a heat transfer system 2600 includes an evaporator 2605 coupled to a cyclical heat exchange system 2610 and an expansion volume 2615 coupled to the evaporator 2605. The vapor channels of the evaporator 2605 feed to a vapor line 2620 that feed a series of channels 2625 of a condenser 2630. The condensed liquid from the condenser 2630 is collected in a liquid return channel 2635. The heat transfer system 2600 also includes fin stock 2640 thermally coupled to the condenser 2630.
[0196] The evaporator 2605 includes a heated wall 2700, a liquid barrier wall 2705, a primary wick 2710 positioned between the heated wall 2700 and an inner side of the liquid barrier wall 2705, vapor removal channels 2715, and liquid flow channels 2720. The liquid barrier wall 2705 is coaxial with the primary wick 2710 and the heated wall 2700. The liquid flow channels 2720 are fed by a liquid return channel 2725 and the vapor removal channels 2715 feed into a vapor outlet 2730.
[0197] The heated wall 2700 intimately contacts the primary wick 2710. The liquid barrier wall 2705 contains working fluid on an inner side of the liquid barrier wall 2705 such that the working fluid flows only along the inner side of the liquid barrier wall 2705. The liquid barrier wall 2705 closes the evaporator's envelope and helps to organize and distribute the working fluid through the liquid flow channels 2720.
[0198] In one implementation, the evaporator 2605 is approximately 2″ tall and the expansion volume 2615 is approximately 1″ in height. The evaporator 2605 and the expansion volume 2615 are wrapped around a portion of the cyclical heat exchange system 2610 having a 4″ outer diameter. The vapor line 2620 has a radius of ⅛″. The cyclical heat exchange system 2610 includes approximately 58 condenser channels 2625, with each condenser channel 2625 having a length of 2″ and a radius of 0.012″, the channels 2625 being spread out such that the width of the condenser 2630 is approximate 40″. The liquid return channel 2725 has a radius of 1/16″. The heat exchanger 2800 (which includes the condenser 2630 and the fin stock 2640 is approximately 40″ long and is wrapped into an inner and outer loop (see FIGS. 30 , 33, and 34) to produce a cylindrical heat exchanger having an outer diameter of approximately 8″. The evaporator 2605 has a cross-sectional width 2750 of approximately ⅛″, as defined by the heated wall 2700 and the liquid barrier wall 2705. The vapor removal channels 2715 have widths of approximately 0.020″ and depths of approximately 0.020″ and are separated from each other by approximately 0.020″ to produce 25 channels per inch.
[0199] As mentioned above, the heat transfer system (such as system 2310) is thermally coupled to the portion (such as portion 2315) of the cyclical heat exchange system. The thermal coupling between the heat transfer system and the portion can be by any suitable method. In one implementation, if the evaporator of the heat transfer system is thermally coupled to the hot side of the cyclical heat exchange system, the evaporator may surround and contact the hot side and the thermal coupling may be enabled by a thermal grease compound applied between the hot side and the evaporator. In another implementation, if the evaporator of the heat transfer system is thermally coupled to the hot side of the cyclical heat exchange system, the evaporator may be constructed integrally with the hot side of the cyclical heat exchange system by forming vapor channels directly into the hot side of the cyclical heat exchange system.
[0200] Referring to FIGS. 30-32 , a heat transfer system 3000 is packaged around a cyclical heat exchange system 3005. The heat transfer system 3000 includes a condenser 3010 surrounding an evaporator 3015. Working fluid that has been vaporized exits the evaporator 3015 through a vapor outlet 3020 connected to the condenser 3010. The condenser 3010 loops around and doubles back inside itself at junction 3025.
[0201] The cyclical heat exchange system 3005 is surrounded about its heat rejection surface 3100 by the evaporator 3015. The evaporator 3015 is in intimate contact with the heat rejection surface 3100. The refrigeration assembly (which is the combination of the cyclical heat exchange system 3005 and the heat transfer system 3000) is mounted in a tube 3205, with a fan 3210 mounted at the end of the tube 3205 to force air through fins 3030 of the condenser 3010 to exhaust channels 3035.
[0202] The evaporator 3015 has a wick 3215 in which working fluid absorbs heat from the heat rejection surface 3100 and changes phase from liquid to vapor. The heat transfer system 3000 includes a reservoir 3220 at the top of the evaporator 3015 that provides an expansion volume. For simplicity of illustration, the evaporator 3015 has been illustrated in this view as a simple hatched block that shows no internal detail. Such internal details are discussed elsewhere in this description.
[0203] The vaporized working fluid exits the evaporator 3015 through the vapor outlet 3020 and enters a vapor line 3040 of the condenser 3010. The working fluid flows downward from the vapor line 3040, through channels 3045 of the condenser 3010, to a liquid return line 3050. As the working fluid flows through the channels 3045 of the condenser 3010 it loses heat, through the fins 3030 to the air passing between the fins, to change phase from vapor to liquid. Air that has passed through the fins 3030 of the condenser 3010 flows away through the exhaust channel 3035. Liquefied working fluid (and possibly some uncondensed vapor) flows from the liquid return line 3050 back into the evaporator 3015 through the liquid return port 3055.
[0204] Referring to FIGS. 33 and 34 , a heat transport system 3300 surrounds a portion of a cyclical heat exchange system 3302 that is surrounded, in turn, by exhaust channels 3305. The heat transport system 3300 includes an evaporator 3310 having an upper portion that surrounds the cyclical heat exchange system 3302. A vapor port 3315 connects the evaporator 3310 to a vapor line 3312 of a condenser 3320. The vapor line 3312 includes an outer region that circles around the evaporator 3310 and then doubles back on itself at junction 3325 to form an inner region that circles back around the evaporator 3310 in the opposite direction. The heat transport system 3300 also includes cooling fins 3330 on the condenser 3320.
[0205] The heat transport system 3300 also includes a liquid return port 3400 that provides a path for condensed working fluid from a liquid line 3405 of the condenser 3320 to return to the evaporator 3310.
[0206] As mentioned above, the interface between the evaporator 3310 and the heat rejection surface of the cyclical heat exchange system 3302 may be implemented according one of several alternative implementations.
[0207] Referring to FIG. 35 , in one implementation, an evaporator 3500 slips over a heat rejection surface 3502 of a cyclical heat exchange system 3505. The evaporator 3500 includes a heated wall 3510, a liquid barrier wall 3515, and a wick 3520 sandwiched between the heated wall 3510 and the liquid barrier wall 3515. The wick 3520 is equipped with vapor channels 3525 and liquid flow channels 3530 are formed at the liquid barrier wall 3515 in simplified form for clarity.
[0208] The evaporator 3500 is slipped over the cyclical heat exchange system 3505 and may be held in place with the use of a clamp 3600 (shown in FIG. 36 ). To aid heat transfer, thermally conductive grease 3535 is disposed between the cyclical heat exchange system 3505 and heated wall 3510 of the evaporator 3500. In an alternative implementation, the vapor channels 3525 are formed in the heated wall 3510 instead of in the wick 3520.
[0209] Referring to FIG. 37 , in another implementation, an evaporator 3700 is fit over a heat rejection surface 3702 of a cyclical heat exchange system 3705 with an interference fit. The evaporator 3700 includes a heated wall 3710, a liquid barrier wall 3715, and a wick 3720 sandwiched between the heated wall 3710 and the liquid barrier wall 3715. The evaporator 3700 is sized to have an interference fit with the heat rejection surface 3702 of the cyclical heat exchange system 3705.
[0210] The evaporator 3700 is heated so that its inner diameter expands to permit it to slip over the unheated heat rejection surface 3702. As the evaporator 3700 cools, it contracts to fix onto the cyclical heat exchange system 3705 in an interference fit relationship. Because of the tightness of the fit, no thermally conductive grease is needed to enhance heat transfer. The wick 3720 is equipped with vapor channels 3725. In an alternative implementation, the vapor channels are formed in the heated wall 3710 instead of in the wick 3720. Liquid flow channels 3730 are formed at the liquid barrier wall 3715 in a simplified form for clarity.
[0211] Referring to FIG. 38 , in another implementation, an evaporator 3800 is fit over a heat rejection surface 3802 of a cyclical heat exchange system 3805 and features previously designed within the evaporator 3800 are now integrally formed within the heat rejection surface 3802. In particular, the evaporator 3800 and the heat rejection surface 3802 are constructed together as an integrated assembly. The heat rejection surface 3802 is modified to have vapor channels 3825; in this way, the heat rejection surface 3802 acts as a heated wall for the evaporator 3800.
[0212] The evaporator 3800 includes a wick 3820 and a liquid barrier wall 3815 formed about the modified heat rejection surface 3802, the wick 3820 and the liquid barrier wall 3815 being integrally bonded to the heat rejection surface 3802 to form the sealed evaporator 3800. Liquid flow channels 3830 are portrayed in a simplified form for clarity. In this way, a hybrid cyclical heat exchange system with an integrated evaporator is formed. This integral construction provides enhanced thermal performance in comparison to the clamp-on construction and the interference fit construction because thermal resistance is reduced between the cyclical heat exchange system 3805 and the wick 3820 of the evaporator 3800.
[0213] Referring to FIG. 29 , graphs 2900 and 2905 show the relationship between a maximum temperature of the surface of the portion of the cyclical heat exchange system that is to be cooled by the heat transfer system and a surface area of the interface between the heat transfer system and the portion of the cyclical heat exchange system to be cooled. The maximum temperature indicates the maximum amount of heat rejection. In graph 2900, the interface between the portion and the heat transfer system is accomplished with a thermal grease compound. In graph 2905, the heat transfer system is made integral with the portion.
[0214] As shown, at an air flow of 300 CFM, if the interface is a thermal grease interface, then the maximum amount of heat rejection would fall within a maximum heat rejection surface temperature 2907 (for example, 70° C.) with a heat exchange surface area 2910 (for example, 100 ft2). When the evaporator is constructed integrally with the portion by forming vapor channels directly in the heat rejection surface, that heat rejection surface would operate below the maximum heat rejection surface temperature of the thermal grease interface with significantly smaller heat exchange surface areas.
[0215] Referring to FIG. 39 , a condenser 3900 is formed with fins 3905, which provide thermal communication between the air or the environment and a vapor line 3910 of the condenser 3900. The vapor line 3910 couples to a vapor outlet 3915 that connects an evaporator 3920 positioned within the condenser 3900.
[0216] Referring to FIGS. 40-43 , in one implementation, the condenser 3900 is laminated and is formed with flow channels that extend through a flat plate 4000 of the condenser 3900 between a vapor head 3925 and a liquid head 3930. Copper is a suitable material for use in making a laminated condenser. The laminated structure condenser 3900 includes a base 4200 having fluid flow channels 4205 (shown in phantom) formed therein and a top layer 4210 is bonded to the base 4200 to cover and seal the fluid flow channels 4205. The fluid flow channels 4205 are designed as trenches formed in the base 4200 and sealed beneath the top layer 4210. The trenches for the fluid flow channels 4205 may be formed by chemical etching, electrochemical etching, mechanical machining, or electrical discharge machining processes.
[0217] Referring to FIGS. 44 and 45 , in another implementation, the condenser 3900 is extruded and small flow channels 4400 extend through a flat plate 4405 of the condenser 3900. Aluminum is a suitable material for use in such an extruded condenser. The extruded micro channel flat plate 4405 extends between a vapor header 4410 and a liquid header 4415. Moreover, corrugated fin stock 4420 is bonded (for example, brazed or epoxied) to both sides of the flat plate 4405.
[0218] Referring to FIG. 46 , a cross-sectional view of one side of a heat transfer system 4600 that is coupled to a cyclical heat exchange system 4605. This view shows relative dimensions that provide for particularly compact packaging of the heat transfer system. In this view, fins 4610 are portrayed as being 90 degrees out of phase for ease of illustration. To cool heat rejection surface 4615 of the cyclical heat exchange system 4605 having a 4-inch diameter, the evaporator 4620 has a thickness of 0.25 inch and the radial thickness of the condenser is 1.75 inches. This provides on overall dimension for the packaging (the combination of the heat transfer system 4600 and the cyclical heat exchange system 4605 of 8 inches.
[0219] As discussed, the evaporator used in the heat transfer system is equipped with a wick. Because a wick is employed within the evaporator of the heat transfer system, the condenser may be positioned at any location relative to the evaporator and relative to gravity. For example, the condenser may be positioned above the evaporator (relative to a gravitational pull), below the evaporator (relative to a gravitational pull), or adjacent the evaporator, thus experiencing the same gravitational pull as the evaporator.
[0220] Other implementations are within the scope of the following claims.
[0221] Notably, the terms Stirling engine, Stirling heat exchange system, and Free Piston Stirling Cooler have been referenced in several implementations above. However, the features and principals described with respect to those implementations also may be applied to other engines capable of conversions between mechanical energy and thermal energy.
[0222] Moreover, the features and principals described above may be applied to any heat engine, which is a thermodynamic system that can undergo a cycle, that is, a sequence of transformations which ultimately return it to its original state. If every transformation in the cycle is reversible, the cycle is reversible and the heat transfers occur in the opposite direction and the amount of work done switches sign. The simplest reversible cycle is a Carnot cycle, which exchanges heat with two heat reservoirs.
Claims
Certificate of Correction present
The claims shown below may not include correction changes. Use the corrected PDF for authoritative text.
What is claimed is:
1. An evaporator for a heat transfer system, the evaporator comprising:
a heated wall;
a liquid barrier wall adjacent to and surrounding the heated wall, the liquid barrier wall and the heated wall being configured to contain working fluid between adjacent sides of the heated wall and the liquid barrier wall;
a primary wick positioned between the adjacent sides of the heated wall and the liquid barrier wall;
a vapor removal channel that is located at an interface between the primary wick and the heated wall;
a liquid flow channel located between the liquid barrier wall and the primary wick;
a secondary wick between the liquid flow channel and the primary wick; and
a vapor vent channel at an interface between the secondary wick and the primary wick.
2. The evaporator of claim 1, wherein the primary wick has a thermal conductivity that is low enough to at least substantially prevent the formation of vapor bubbles in the liquid flow channel caused by leakage of heat from the heated wall, through the primary wick, toward the liquid barrier wall.
3. The evaporator of claim 1, wherein the heated wall is defined so as to accommodate the vapor removal channel.
4. The evaporator of claim 1, wherein the interface between the primary wick and the adjacent side of the heated wall is defined so as to accommodate the vapor removal channel.
5. The evaporator of claim 1, wherein a cross section of the vapor removal channel is sufficient to maintain a pressure difference between the vapor removal channel and the liquid flow channel across the primary wick.
6. The evaporator of claim 1, wherein the heated wall is in intimate contact with the primary wick.
7. The evaporator of claim 1, wherein a thickness of the heated wall is selected to ensure at least substantially complete vaporization at the interface between the primary wick and the heated wall.
8. The evaporator of claim 1, wherein the liquid flow channel supplies the primary wick with liquid from a liquid inlet.
9. The evaporator of claim 8, wherein the liquid flow channel is configured to supply the primary wick with enough liquid to offset liquid vaporized at the interface between the primary wick and the heated wall and liquid vaporized at the liquid baffler wall.
10. The evaporator of claim 1, wherein the secondary wick comprises an opening wherein at least one vapor bubble formed within the vapor vent channel is swept through the secondary wick and through the liquid flow channel.
11. The evaporator of claim 1, wherein the vapor vent channel delivers vapor that has vaporized within the primary wick away from the primary wick.
12. The evaporator of claim 1, wherein the primary wick, the heated wall, and the liquid barrier wall are annular and coaxial such that the heated wall is inside the primary wick and the primary wick is inside the liquid barrier wall.
13. A heat transfer system comprising:
an evaporator including:
a heated wall;
a liquid barrier wall adjacent to and surrounding the heated wall, the liquid barrier wall and the heated wall being configured to contain working fluid between adjacent sides of the heated wall and the liquid barrier wall;
a primary wick positioned between the adjacent sides of the heated wall and the liquid barrier wall;
a vapor removal channel that is located at an interface between the primary wick and the heated wall, the vapor removal channel extending to a vapor outlet;
a liquid flow channel located between the liquid barrier wall and the primary wick, the liquid flow channel receiving liquid from a liquid inlet;
a secondary wick between the liquid flow channel and the primary wick; and
a vapor vent channel at an interface between the secondary wick and the primary wick;
a condenser having a vapor inlet and a liquid outlet;
a vapor line providing fluid communication between the vapor outlet and the vapor inlet; and
a liquid return line providing fluid communication between the liquid outlet and the liquid inlet.
14. The heat transfer system of claim 13, further comprising a reservoir in the liquid return line.
15. The heat transfer system of claim 14, wherein the reservoir comprises heat exchanger fins to cold bias the reservoir.
16. The heat transfer system of claim 13, wherein the secondary wick comprises an opening wherein at least one vapor bubble formed within the vapor vent channel is swept through the secondary wick, through the liquid flow channel, and into the reservoir.
17. The heat transfer system of claim 13, wherein the evaporator is annular such that the heated wall is inside the primary wick and the primary wick is inside the liquid baffler wall.
18. The heat transfer system of claim 13, wherein the condenser is configured to subcool the liquid returning into the evaporator.
19. The heat transfer system of claim 18, wherein the condenser is configured to subcool the liquid to a temperature to balance heat leakage through the primary wick.
20. The heat transfer system of claim 13, wherein the heated wall contacts a hot side of a Stirling cooling machine.
Patent Citations (78)
| Patent | Date | Inventor | Cited By |
|---|---|---|---|
| US3490718(A) | 1970-01-01 | Vary | Applicant |
| US3613778(A) | 1971-10-01 | Feldman, Jr. | Applicant |
| US3661202(A) | 1972-05-01 | Moore, Jr. | Applicant |
| US3677336(A) | 1972-07-01 | Moore, Jr. | Applicant |
| US3734173(A) | 1973-05-01 | Moritz | Applicant |
| US3756903(A) | 1973-09-01 | Jones | Applicant |
| US3792318(A) | 1974-02-01 | Fries et al. | Applicant |
| US3803688(A) | 1974-04-01 | Peck | Applicant |
| US3884293(A) | 1975-05-01 | Pessolano et al. | Applicant |
| US4005297(A) | 1977-01-01 | Cleaveland | Applicant |
| US4046190(A) | 1977-09-01 | Marcus et al. | Applicant |
| US4087893(A) | 1978-05-01 | Sata et al. | Applicant |
| US4116266(A) | 1978-09-01 | Sawata et al. | Applicant |
| US4170262(A) | 1979-10-01 | Marcus et al. | Applicant |
| US4467861(A) | 1984-08-01 | Kiseev et al. | Examiner |
| US4470450(A) | 1984-09-01 | Bizzell et al. | Applicant |
| US4503483(A) | 1985-03-01 | Basiulis | Applicant |
| US4685512(A) | 1987-08-01 | Edelstein et al. | Applicant |
| US4770238(A) | 1988-09-01 | Owen | Applicant |
| US4819719(A) | 1989-04-01 | Grote et al. | Applicant |
| US4830718(A) | 1989-05-01 | Stauffer | Applicant |
| US4862708(A) | 1989-09-01 | Basiulis | Applicant |
| US4869313(A) | 1989-09-01 | Fredley | Examiner |
| US4883116(A) | 1989-11-01 | Seidenberg et al. | Applicant |
| US4890668(A) | 1990-01-01 | Cima | Applicant |
| US4934160(A) | 1990-06-01 | Mueller | Examiner |
| US5002122(A) | 1991-03-01 | Sarraf et al. | Applicant |
| US5016705(A) | 1991-05-01 | Bahrle et al. | Examiner |
| US5103897(A) | 1992-04-01 | Cullimore et al. | Applicant |
| US5303768(A) | 1994-04-01 | Alario et al. | Applicant |
| US5335720(A) | 1994-08-01 | Ogushi et al. | Applicant |
| US5642776(A) | 1997-07-01 | Meyer, IV et al. | Applicant |
| US5725049(A) | 1998-03-01 | Swanson et al. | Applicant |
| US5761037(A) | 1998-06-01 | Anderson et al. | Applicant |
| US5771967(A) | 1998-06-01 | Hyman | Applicant |
| US5816313(A) | 1998-10-01 | Baker | Applicant |
| US5842513(A) | 1998-12-01 | Maciaszek et al. | Applicant |
| US5899265(A) | 1999-05-01 | Schneider et al. | Applicant |
| US5944092(A) | 1999-08-01 | Van Oost | Applicant |
| US5950710(A) | 1999-09-01 | Liu | Applicant |
| US5966957(A) | 1999-10-01 | Malhammar et al. | Applicant |
| US6058711(A) | 2000-05-01 | Maciaszek et al. | Applicant |
| US6227288(B1) | 2001-05-01 | Gluck et al. | Examiner |
| US6330907(B1) | 2001-12-01 | Ogushi et al. | Applicant |
| US6381135(B1) | 2002-04-01 | Prasher et al. | Applicant |
| US6382309(B1) | 2002-05-01 | Kroliczek et al. | Applicant |
| US6415627(B1) | 2002-07-01 | Pfister et al. | Examiner |
| US6450132(B1) | 2002-09-01 | Yao et al. | Applicant |
| US6533029(B1) | 2003-03-01 | Phillips | Examiner |
| US6591902(B1) | 2003-07-01 | Trent | Applicant |
| US6596035(B2) | 2003-07-01 | Gutkowski et al. | Applicant |
| US6615912(B2) | 2003-09-01 | Garner | Applicant |
| US6810946(B2) | 2004-11-01 | Hoang | Applicant |
| US6840304(B1) | 2005-01-01 | Kobayashi et al. | Examiner |
| US7004240(B1) | 2006-02-01 | Kroliczek et al. | Applicant |
| US7251889(B2) | 2007-08-01 | Kroliczek et al. | Examiner |
| US2002/0007937(A1) | 2002-01-01 | Kroliczek et al. | Applicant |
| US2003/0051857(A1) | 2003-03-01 | Cluzet et al. | Applicant |
| US2004/0182550(A1) | 2004-09-01 | Kroliczek et al. | Applicant |
| US2004/0206479(A1) | 2004-10-01 | Kroliczek et al. | Applicant |
| DE19941398 | 2000-08-01 | Applicant | |
| EP210337 | 1987-02-01 | Applicant | |
| EP355921(B1) | 1994-07-01 | Applicant | |
| EP700737(A2) | 1996-03-01 | Applicant | |
| EP987509(A1) | 2000-03-01 | Applicant | |
| EP1084688(A3) | 2001-08-01 | Applicant | |
| HU212748(B) | 1995-09-01 | Applicant | |
| JP63036862 | 1988-03-01 | Applicant | |
| JP2000-055577 | 2000-02-01 | Applicant | |
| JP200241089 | 2000-09-01 | Applicant | |
| RU2098733 | 1995-03-01 | Applicant | |
| RU1834470(A1) | 1995-07-01 | Applicant | |
| SU505858 | 1976-05-01 | Applicant | |
| SU1467354 | 1987-01-01 | Applicant | |
| WO2/10661(A1) | 2002-02-01 | Applicant | |
| WO3054469 | 2003-07-01 | Applicant | |
| WO2004031675 | 2004-04-01 | Applicant | |
| WO2004040218 | 2004-05-01 | Applicant |
Non-Patent Literature (39)
- PCT International Preliminary Examination Report (Application No. PCT/US03/34165), mailed Mar. 8, 2007, 3 total pages.Applicant
- “A high power spacecraft thermal management system,” J. Ku, et al., AIAA-1988-2702, Thermophysics, Plasmadynamics and Lasers Conference, San Antonio, TX, Jun. 27-29, 1988, 12 pages.Applicant
- “Across-Gimbal and Miniaturized Cryogenic Loop Heat Pipes,” Bugby, D. et al., CP654, Space Technology and Applications International Forum-STAIF 2003, edited by M.S. El-Genk, American Institute of Physics, 2003, pp. 218-226.Applicant
- “Advanced Components for Cryogenic Integration,” Bugby, D. et al., Cryocoolers 12, edited by R.G. Ross, Jr., Kluwer Academic/Plenum Publishers, 2003, pp. 693-708.Applicant
- “Advanced Components for Cryogenic Integration,” D. Bugby et al, Proceedings of the 12th International Cryocooler Conference, held Jun. 18-20, 2002, in Cambridge MA., 15 pages.Applicant
- “Advanced Components and Techniques for Cryogenic Integration,” D. Bugby et al., Environmental systems—International conference; 31st, Society of Automotive Engineers New York, 2001-01-2378, Orlando, FL 2001; Jul (200107), 9 pages.Applicant
- “Advanced Components and Techniques for Cryogenic Integration,” D. Bugby et al., presented at 2002 Spacecraft Thermal Control Symposium by Swales Aerospace, El Segundo, CA, Mar. 2002, 14 pages.Applicant
- “An Improved High Power Hybrid Capillary Pumped Loop,” J. Ku et al., paper submitted to SAE 19th Intersociety Conference on Environment Systems, SAE 891566, San Diego, CA, Jul. 24-27, 1989, 10 pages.Applicant
- “Design and Experimental Results of the HPCPL,” Van Oost et al., ESTEC CPL-96 Workshop, Noordwijk, Netherlands, 1996, 29 pages.Applicant
- “Design and Test of a Proof-of-Concept Advanced Capillary Pumped Loop,” Triem T. Hoang, Society of Automotive Engineers, presented at the 27th Environmental systems International conference, New York, 1997, Paper 972326, 6 pages.Applicant
- “Design and Testing of a High Power Spacecraft Thermal Management System,” McCabe, Jr., Michael E. et al., National Aeronautics and Space Administration (NASA), NASA Technical Memorandum 4051, Scientific and Technical Information Division, 1988, 107 pages.Applicant
- “Development and Testing of a Gimbal Thermal Transport System,” D. Bugby et al., Proceedings of the 11th International Cryocooler Conference, held Jun. 20-22, 2000, in Keystone, Colorado, 11 pages.Applicant
- “Development of a Cryogenic Loop Heat Pipe (CLHP) for Passive Optical Bench Cooling Applications,” James Yun, et al., 32nd International Conference on Environmental Systems (ICES-2002), Society of Automotive Engineers Paper No. 2002-01-2507, San Antonio, Texas, 2002, 9 pages.Applicant
- “Development of an Advanced Capillary Pumped Loop,” Triem T. Hoang et al., Society of Automotive Engineers, presented at the 27th Environmental systems International conference, New York, 1997, Paper 972325, 6 pages.Applicant
- “Development of Advanced Cryogenic Integration Solutions,” D. Bugby et al., presented at the 10th International Cryocoolers Conference on May 26-28, 1998 in Monterey, CA and published in “Cryocoolers 10,” by Ron Ross, Jr., Kluwer Academic/Plenum Publishers, NY 1999, 17 pages.Applicant
- “Hydrogen Loop Pipe Design & Test Results,” O'Connell et al., presented at 2002 Spacecraft Thermal Control Symposium by TTH Research, El Segundo, CA, Mar. 2002, 14 pages.Applicant
- “Multiple Evaporator Loop Heat Pipe,” James Yun, et al., Society of Automotive Engineers, 2000-01-2410, 30th International Conference on Environmental Systems, Jul. 10-13, 2000, 10 pages.Applicant
- “Recent Advances in Capillary Pumped Loop Technology,” J. Ku, 1997 National Heat Transfer Conference, Baltimore, MD, Aug. 10-12, 1997, AIAA 97-3870, 22 pages.Applicant
- “Testing of a Capillary Pumped Loop with Multiple parallel starter pumps,” J. Ku et al, SAE Paper No. 972329, 1997.Applicant
- “The Hybrid Capillary Pumped Loop,” J. Ku et al., paper submitted to SAE 18th Intersociety Conference on Environmental Systems, SAE 881083, San Francisco, CA, Jul. 11-13, 1988, 11 pages.Applicant
- Jentung Ku, “Operational Characteristics of Loop Heat Pipes”, NASA Goddard Space Flight Center; SAE Paper 99-01-2007, 29th International Conference on Environmental Systems, Denver, Colorado, Jul. 12-15, 1999; Society of Automotive Engineers, Inc.Applicant
- Jane Baumann et al., “A methodology for enveloping reliable start-up of LHPs”, AIAA Paper 2000-2285 (AIAA Accession No. 33681), AIAA Thermophysics Conference, 34th, Denver, CO, Jun. 19-22, 2000.Applicant
- W. B. Bienert et al., “The Proof-Of-Feasibility of Multiple Evaporator Loop Heat Pipes”, 6th European Symposium on Environmental Systems, May 1997, 6 pages.Applicant
- S. Yun et al., “Design and Test Results of Multi-Evaporator Loop Heat Pipes”, SAE Paper No. 1999-01-2051, 29th International Conference on Environmental Systems, Jul. 1999, 7 pages.Applicant
- Stephane Van Oost et al., “Test Results of Reliable and Very High Capillary Multi-Evaporators/Condenser Loop”, 25th International Conference on Environmental Systems, Jul. 10-13, 1995, 12 pages.Applicant
- E. Yu Kotlyarov et al., “Methods of Increase of the Evaporators Reliability for Loop Heat Pipes and Capillary Pumped Loops”, 24th International Conference on Environmental Systems, Jun. 20-23, 1994, 15 pages.Applicant
- Hoang, “Advanced Capillary Pumped Loop (A-CPL) Project Summary” Contract No. NAS5-98103, Mar. 1994, pp. 1-37.Applicant
- Martien Janssen et al., “Measurement and application of performance characteristics of a Free Piston Stirling Cooler”, 9th International Refrigeration and Air Conditioning Conference, Jul. 16-19, 2002, 8 pages.Applicant
- Yong-Rak Kwon et al., “Operational Characteristics of Stirling Machinery”, International Congress of Refrigeration, Aug. 17-22, 2003, 8 pages.Applicant
- David M. Berchowitz et al., “Design and Testing of a 40 W Free-Piston Stirling Cycle Cooling Unit”, 20th International Conference of Refrigeration, IIR/IIF, Sydney, 1999, 7 pages.Applicant
- D.M. Berchowitz Ph. D., “Maximized Performance of Stirling Cycle Refrigerators”, Natural working fluids '98 IIR—Gustav Lorentzen Conference: Oslo, Norway, Jun. 2-5, 1998, Fluides actifs naturels conference IIF—Gustav Lorentzen, Journal: Science et technique du froid, 1998 (4) 422-429.Applicant
- David M. Berchowitz, “Free-Piston Rankine Compression and Stirling Cycle Machines for Domestic Refrigeration”, Presented at the Greenpeace Ozon Safe Conference, Washington, DC, Oct. 18-19, 1993.Applicant
- Stephen C. Wetty and Fernando Cueva, “Energy Efficient Freezer Installation Using Natural Working Fluids and a Free Piston Stirling Cooler” VI Congreso Iberoamericano De Aire Acondicionado Y Refrigeracion, CIAR 2001, Trabajo No. 96, pp. 199-208, Aug. 15-17, 2001.Applicant
- Emre Oguz et al., “Experimental Investigation Of a Stirling Cycle Cooled Domestic Refrigerator”, 9th Proceedings of the International Refrigeration and Air Conditioning Conference at Purdue, 2002; 9th; vol. 2, pp. 777-784.Applicant
- Seon-Young Kim et al., “The Application of Stirling Cooler to Refrigeration”, IECEC-97-Intersociety Energy Conversion Engineering Conference, 1997, Conference 32, vol. 2, pp. 1023-1026.Applicant
- D.M. Berchowitz et al. “Recent Advances in Stirling Cycle Refrigeration”, 1995, 19th International Conference of Refrigeration, The Hague, The Netherlands, 8 pages.Applicant
- Russian Office Action for related Russian Application No. 2005116246, issued Oct. 9, 2008.Applicant
- European Search Report for Application No. EP 04016584 dated May 15, 2006, 4 pages.Applicant
- International Search Report issued in International Application No. PCT/US04/35548, Jun. 13, 2005.Applicant