US20160231063A1 - Thermosyphon Configuration for Cascade Refrigeration Systems - Google Patents
Thermosyphon Configuration for Cascade Refrigeration Systems Download PDFInfo
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- US20160231063A1 US20160231063A1 US15/007,251 US201615007251A US2016231063A1 US 20160231063 A1 US20160231063 A1 US 20160231063A1 US 201615007251 A US201615007251 A US 201615007251A US 2016231063 A1 US2016231063 A1 US 2016231063A1
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- thermosyphon
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B41/00—Fluid-circulation arrangements
- F25B41/40—Fluid line arrangements
- F25B41/42—Arrangements for diverging or converging flows, e.g. branch lines or junctions
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B41/00—Fluid-circulation arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B7/00—Compression machines, plants or systems, with cascade operation, i.e. with two or more circuits, the heat from the condenser of one circuit being absorbed by the evaporator of the next circuit
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2400/00—General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
- F25B2400/23—Separators
Definitions
- the present application and the resultant patent relate generally to refrigeration systems and more particularly relate to a cascade refrigeration system using a thermosyphon in communication with a cascade evaporator-condenser the low side cooling cycle components.
- Cascade refrigeration systems generally include a first side cooling cycle, or a high side cooling cycle, and a second side cooling cycle, or a low side cooling cycle.
- the two cooling cycles interface through a common heat exchanger, i.e., a cascade evaporator-condenser.
- the cascade refrigeration system may provide cooling at very low temperatures in a highly efficient manner.
- an improved refrigeration system such as a cascade refrigeration system that provides cooling with increased efficiency with natural or any type of refrigerants.
- Such an improved refrigeration system may accommodate the high pressures needed for low temperature cascade cooling in an efficient, reliable, and safe manner.
- thermosyphon for use with a refrigeration system.
- the thermosyphon may include a primary flow inlet, an angled secondary flow inlet, and a mixed flow outlet.
- the angled secondary flow inlet may include an angle ⁇ 1 of about forty-five degrees or less with respect to the mixed flow outlet.
- the angled flow may improve the mass flow rate or reduce the pressure of the primary inlet flow and the mixed outlet flow as compared to a perpendicular orientation.
- the present application and the resultant patent further provide a method of improving a mass flow rate or reducing a pressure loss of a refrigerant to a cascade evaporator-condenser.
- the method may include the steps of providing a thermosyphon with an outlet in communication with the cascade evaporator-condenser, providing a primary refrigerant flow from a first source, providing a secondary refrigerant flow from a second source, mixing the primary refrigerant flow and the secondary refrigerant flow at an angle less than about ninety degrees, and providing the mixed refrigerant flow to the cascade evaporator-condenser via the thermosyphon outlet.
- thermosyphon for use with a refrigeration system.
- the thermosyphon may include a tank inlet in communication with a liquid vapor separator tank, an angled compressor inlet in communication with one or more compressors, and a cascade outlet in communication with a cascade evaporator-condenser.
- the angled compressor inlet may include an angle of about forty-five degrees or less with respect to the cascade outlet.
- FIG. 1 is a schematic diagram of a known cascade refrigeration system with a high side cycle and a low side cycle.
- FIG. 2 is a schematic diagram of a thermosyphon configuration as used in a known cascade refrigeration system.
- FIG. 3 is an alternative embodiment of a known thermosyphon configuration.
- FIG. 4 is a thermosyphon configuration as may be described herein with an improved mass flow rate or reduced pressure loss.
- FIG. 5 is an alternative embodiment of a thermosyphon configuration as may be described herein.
- FIG. 6 is an alternative embodiment of a thermosyphon configuration as may be described herein.
- FIG. 1 shows an example of a cascade refrigeration system 100 .
- the cascade refrigeration system 100 may be used to cool any type of enclosure for use in, for example, supermarkets, cold storage, and the like.
- the cascade refrigeration system 100 also may be applicable to other types of heating, ventilation, and air conditioning applications and/or different types of commercial and/or industrial applications.
- the overall cascade refrigeration system 100 may have any suitable size or capacity. Other types of refrigeration systems, cycled, and components also may be used herein.
- the cascade refrigeration system 100 may include a first or a high side cycle 110 and a second or a low side cycle 120 .
- the high side cycle 110 may include one or more high side compressors 130 , a high side oil separator 140 , a high side condenser 150 , a high side receiver 160 , and a high side expansion device 170 .
- the high side cycle 110 also may include a suction/liquid heat exchanger 180 and a suction accumulator 190 .
- the high side cycle 110 may include a flow of a refrigerant 200 .
- the refrigerant 200 may include a flow of ammonia or other type of a refrigerant.
- the high side cycle 110 components may have any suitable size, shape, configuration, or capacity. The high side cycle 110 may use other and additional components and configurations herein.
- the low side cycle 120 similarly may include one or more low side compressors 210 , a low side oil separator 220 , a low side liquid vapor separator tank 230 , one or more low side expansion devices 240 , and one or more low side evaporators 250 .
- the low side cycle 120 may include a medium temperature loop 260 with a pump 270 and a number of flow valves 280 as well as a low temperature loop 290 .
- An accumulator 300 also may be used therein.
- the low side cycle 120 may include a flow of a refrigerant 310 .
- the refrigerant 310 may include a flow of carbon dioxide or other type of a refrigerant.
- the low side cycle 120 components may have any suitable size, shape, configuration, or capacity. The low side cycle 120 may use other and additional components and configurations herein.
- the two cycles 110 , 120 may interface through a cascade evaporator/condenser 320 .
- the respective flows of the refrigerants 200 , 310 may exchange heat via the cascade evaporator/condenser 320 .
- the cascade evaporator/condenser 320 may have any suitable size shape, configuration, or capacity. Other components and other configurations may be used herein.
- the refrigerant 200 may be compressed by the high side compressors 130 and condensed in the high side condenser 150 .
- the refrigerant 200 may be stored in the high side receiver 160 and may be withdrawn as needed to satisfy the load on the cascade evaporator/condenser 320 .
- the refrigerant 200 then may pass through the suction/liquid heat exchanger 180 , the high side expansion device 170 and the cascade evaporator/condenser 320 .
- the refrigerant 200 again passes through the suction/liquid heat exchanger 180 and returns to the high side compressors 130 .
- the suction/liquid heat exchanger 180 may be used to sub-cool the refrigerant 200 before entry into the cascade evaporator/condenser 320 .
- Other components and other configurations may be used herein.
- the low side cycle 120 may be similar.
- the carbon dioxide based refrigerant 310 may be compressed by the low side compressors 210 and then pass through the cascade evaporator/condenser 320 .
- the refrigerant 310 may be stored within the low side liquid vapor separator tank 230 and withdrawn as needed.
- the refrigerant 310 may pass through one or more low side expansion devices 240 and one or more low side evaporators 250 .
- the low side cycle 120 may be separated into the low temperature loop 290 and the medium temperature loop 260 .
- Other components and other configurations may be used herein.
- the low side cycle 120 also may use a thermosyphon 330 .
- the thermosyphon 330 provides for the circulation of a fluid, in this case the refrigerant 310 , based upon thermal gradients as opposed to mechanical devices such as a pump and the like.
- the thermosyphon 330 may have a tank inlet 340 in communication with the low side liquid vapor separator tank 230 , a compressor inlet 350 in communication with the low side compressors 210 , and a cascade outlet 360 in communication with the cascade evaporator-condenser 320 .
- the liquid/gas flow of the carbon dioxide refrigerant 310 may be diverted to the low side liquid vapor separator tank 230 where the liquid and vapor may separate therein.
- the vapor portion may be routed to the cascade evaporator-condenser 320 through the thermosyphon 330 and mixed with the vapor exiting the low side compressors 210 so as to condense the vapor to a liquid.
- Other components and other configurations may be used herein.
- FIGS. 1 and 2 show an example of a conventional configuration of the thermosyphon 330 .
- the compressor inlet 350 may be in line with the cascade outlet 360 .
- the tank inlet 340 may merge in a perpendicular relationship at approximately a ninety degree (90°) angle so as to provide the thermosyphon 330 with a substantial tank “T” like shape 370 .
- FIG. 3 shows a similar configuration in which the tank inlet 340 is in line with the cascade outlet 360 and the compressor inlet 350 merges perpendicularly for a compressor “T” like shape 380 . In either orientation, the flows merge at about the perpendicular angle.
- the flow from the low side liquid vapor separator tank 230 through the tank inlet 340 may be considered a primary flow 390 .
- the flow from the compressors 210 to the compressor inlet 350 may be considered a secondary flow 400 .
- blocking the respective flows through the pressure drop sensitive thermosyphon 330 may be an operational and an efficiency issue.
- the primary flow 390 through the tank inlet 340 may be at about 435.07 psia (about 3000 kpa) with a temperature of about 22 degrees Fahrenheit (about ⁇ 5.5 degrees Celsius) and with a mass flow rate of about 0.17 or 0.18 kg/s.
- the secondary flow 400 through the compressor 360 may be at about 145 degrees Fahrenheit (about 63 degrees Celsius) and with a mass flow rate of about 0.09 kg/s.
- a mixed outlet flow 410 at the cascade outlet 360 may be at about 434.87 psia (about 2998 kpa), about 45 degrees Fahrenheit (about 7.2 degrees Celsius), and with a mass flow rate of about 0.26 or 0.27 kg/s.
- Other pressures, temperatures, mass flow rates, and other parameters may be used herein.
- FIG. 4 shows an example of a thermosyphon 420 as may be described herein.
- the thermosyphon 420 may have a tank inlet 430 that is in line with a cascade outlet 440 .
- the thermosyphon 420 may include an angled inlet compressor 450 .
- the angled compressor inlet 450 may be positioned at an angle ⁇ 1 with respect to the tank inlet 430 or the centerline of the cascade outlet 440 .
- the angle ⁇ 1 preferably may range from about more than about zero degrees (0°) to about forty-five degrees (45°) or so. Other angles may be used herein.
- Other components and other configurations may be used herein.
- FIG. 5 shows a further example of a thermosyphon 460 as may be described herein.
- the thermosyphon 460 may include an angled tank inlet 470 and/or an angled compressor inlet 480 .
- the inlets 470 , 480 then may merge into a cascade outlet 490 for a substantial “Y” like shape.
- the angled tank inlet 470 may be positioned at an angle of ⁇ 2 with respect to the centerline of the cascade outlet 490 .
- the angle ⁇ 2 preferably may range from about more than about zero degrees (0°) to about forty-five degrees (45°) or so. Other angles may be used herein.
- the angled compressor inlet 480 also may use the angle ⁇ 1 similar to that described above. Specifically, the angles ⁇ 1 and ⁇ 2 may be the same or different. Other components and other configurations also may be used herein.
- the following chart shows the mass flow rate changes with respect to the thermosyphon 330 of FIGS. 2 and 3 and the thermosyphons 420 , 460 of FIGS. 4 and 5 .
- the comparison assumes the same pressure and temperature at the tank inlet, the same mass flow rate and temperature at the compressor inlet, and the same pressure and temperature at the cascade outlet.
- the mass flow rate into the tank inlet and out of the cascade outlet will vary.
- the angle ⁇ 1 was varied from six degrees (6°) to about ninety degrees (90°).
- angle ⁇ 1 varied from about ten degrees) (10° to about thirty degrees (30°) and ⁇ 2 varied from about three degrees (3°) to about thirty degrees (30°).
- the respective changes in mass flow rate thus are shown with respect to kilograms per second.
- FIG. ⁇ 1- ⁇ 2 (kg/s) (kg/s) (kg/s) from FIG. 2
- 0.09 0.17 0.26 3 0.09 0.18 0.27 5.46 4 6° 0.09 0.24 0.33 41.17 11° 0.09 0.24 0.33 41.17 15° 0.09 0.23 0.32 35.29 30° 0.09 0.23 0.32 35.29 45° 0.09 0.23 0.32 35.29 5 90° 0.09 0.09 0.18 ⁇ 47.03 10°-10° 0.09 0.22 0.31 29.70 15°-15° 0.09 0.20 0.29 18.29 30°-30° 0.09 0.21 0.30 22.79 14°-3° 0.09 0.22 0.31 32.34
- the tank inlet flow rate and the cascade outlet flow rate thus varied and improved with respect to the perpendicular configuration of FIGS. 2 and 3 .
- the use of an angle of about six degrees (6°) to about eleven degrees (11°) improved the mass flow rate at the cascade outlet from about 0.26 kg/s to about 0.33 kg/3 or an increase of about forty-one percent (41%).
- Varying the angle of the secondary flow 400 with respect to the primary flow 390 thus provides an enhanced primary flow rate as compared to the perpendicular angle arrangement and/or a decreased pressure drop along the primary flow for the same inlet velocity.
- FIG. 6 shows a further embodiment of a thermosyphon 500 as may be described herein.
- the thermosyphon 500 may include a tank inlet 510 and an inline cascade outlet 520 .
- the thermosyphon 500 may include an angled compressor inlet 530 .
- the angle ⁇ 1 of the angled compressor inlet 530 thus may vary.
- the angled compressor inlet 530 may have a variable diameter 540 .
- the diameter of the variable diameter 540 may vary. Varying angles and diameters also may be used for the tank inlet 510 .
- the tank inlet 510 may have a diameter of about 13 ⁇ 8 inches (about 34.9 millimeters) or so. Other components and other configurations may be used herein.
- the following chart shows examples in varying the angle ⁇ 1 as well as the diameter from about 0.4 inch (about 10.2 millimeters) to about one (1) inch (about 25.4 millimeters) given the constant tank inlet 510 described above.
- variable diameter 540 of about 10.2 millimeters with an angle ⁇ 1 of about thirty degrees for the angled compressor inlet 530 thus results in more than a 100% improvement over the FIG. 2 baseline.
- a higher secondary flow from the compressors 210 may draw more of the refrigerant 310 from the liquid vapor separator tank 230 without obstructing the flow given a jet of a smaller diameter.
- the ratio of the diameters between the angled compressor inlet 530 and the tank inlet varied from about 0.7 to about 0.3 with at least a 0.5 ratio being preferred.
- variable diameter 540 also may be dynamically set depending upon operational parameters.
- the variable diameter 540 may vary depending upon the load on the overall system and the like. Other parameters may be considered herein.
- thermosyphons herein have been focused on the use of the carbon dioxide refrigerant 310 , the thermosyphons described herein may be used to merge any type of primary and secondary flows.
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Abstract
Description
- The present application is a non-provisional application claim priority to U.S. Provisional Application Ser. No. 62/114,603, filed on Feb. 11, 2105. U.S. Provisional Application Ser. No. 62/114,603 is incorporated by reference herein in full.
- The present application and the resultant patent relate generally to refrigeration systems and more particularly relate to a cascade refrigeration system using a thermosyphon in communication with a cascade evaporator-condenser the low side cooling cycle components.
- Cascade refrigeration systems generally include a first side cooling cycle, or a high side cooling cycle, and a second side cooling cycle, or a low side cooling cycle. The two cooling cycles interface through a common heat exchanger, i.e., a cascade evaporator-condenser. The cascade refrigeration system may provide cooling at very low temperatures in a highly efficient manner.
- Current refrigeration trends promote the use of ammonia, carbon dioxide, and other types of natural refrigerants instead of conventional hydrofluorocarbon based refrigerants. Cascade refrigeration systems may use ammonia in the high cycle and carbon dioxide in the low cycle. Moreover, there is an interest in improving the overall efficiency of such natural refrigerant based refrigeration systems at least as compared to the conventional hydrofluorocarbon based systems.
- There is thus a desire for an improved refrigeration system such as a cascade refrigeration system that provides cooling with increased efficiency with natural or any type of refrigerants. Such an improved refrigeration system may accommodate the high pressures needed for low temperature cascade cooling in an efficient, reliable, and safe manner.
- The present application and the resultant patent thus provide a thermosyphon for use with a refrigeration system. The thermosyphon may include a primary flow inlet, an angled secondary flow inlet, and a mixed flow outlet. The angled secondary flow inlet may include an angle θ1 of about forty-five degrees or less with respect to the mixed flow outlet. The angled flow may improve the mass flow rate or reduce the pressure of the primary inlet flow and the mixed outlet flow as compared to a perpendicular orientation.
- The present application and the resultant patent further provide a method of improving a mass flow rate or reducing a pressure loss of a refrigerant to a cascade evaporator-condenser. The method may include the steps of providing a thermosyphon with an outlet in communication with the cascade evaporator-condenser, providing a primary refrigerant flow from a first source, providing a secondary refrigerant flow from a second source, mixing the primary refrigerant flow and the secondary refrigerant flow at an angle less than about ninety degrees, and providing the mixed refrigerant flow to the cascade evaporator-condenser via the thermosyphon outlet.
- The present application and the resultant patent further provide a thermosyphon for use with a refrigeration system. The thermosyphon may include a tank inlet in communication with a liquid vapor separator tank, an angled compressor inlet in communication with one or more compressors, and a cascade outlet in communication with a cascade evaporator-condenser. The angled compressor inlet may include an angle of about forty-five degrees or less with respect to the cascade outlet.
- These and other features and improvements of the present application and the resultant patent will become apparent to one of ordinary skill in the art upon review of the following detailed description when taken in conjunction with the several drawings and the appended claims.
-
FIG. 1 is a schematic diagram of a known cascade refrigeration system with a high side cycle and a low side cycle. -
FIG. 2 is a schematic diagram of a thermosyphon configuration as used in a known cascade refrigeration system. -
FIG. 3 is an alternative embodiment of a known thermosyphon configuration. -
FIG. 4 is a thermosyphon configuration as may be described herein with an improved mass flow rate or reduced pressure loss. -
FIG. 5 is an alternative embodiment of a thermosyphon configuration as may be described herein. -
FIG. 6 is an alternative embodiment of a thermosyphon configuration as may be described herein. - Referring now to the drawings, in which like numerals refer to like elements throughout the several views,
FIG. 1 shows an example of acascade refrigeration system 100. Thecascade refrigeration system 100 may be used to cool any type of enclosure for use in, for example, supermarkets, cold storage, and the like. Thecascade refrigeration system 100 also may be applicable to other types of heating, ventilation, and air conditioning applications and/or different types of commercial and/or industrial applications. The overallcascade refrigeration system 100 may have any suitable size or capacity. Other types of refrigeration systems, cycled, and components also may be used herein. - Generally described, the
cascade refrigeration system 100 may include a first or ahigh side cycle 110 and a second or alow side cycle 120. Thehigh side cycle 110 may include one or morehigh side compressors 130, a highside oil separator 140, ahigh side condenser 150, ahigh side receiver 160, and a highside expansion device 170. Thehigh side cycle 110 also may include a suction/liquid heat exchanger 180 and asuction accumulator 190. Thehigh side cycle 110 may include a flow of arefrigerant 200. Therefrigerant 200 may include a flow of ammonia or other type of a refrigerant. Thehigh side cycle 110 components may have any suitable size, shape, configuration, or capacity. Thehigh side cycle 110 may use other and additional components and configurations herein. - The
low side cycle 120 similarly may include one or morelow side compressors 210, a lowside oil separator 220, a low side liquidvapor separator tank 230, one or more lowside expansion devices 240, and one or morelow side evaporators 250. Thelow side cycle 120 may include amedium temperature loop 260 with apump 270 and a number offlow valves 280 as well as alow temperature loop 290. Anaccumulator 300 also may be used therein. Thelow side cycle 120 may include a flow of arefrigerant 310. Therefrigerant 310 may include a flow of carbon dioxide or other type of a refrigerant. Thelow side cycle 120 components may have any suitable size, shape, configuration, or capacity. Thelow side cycle 120 may use other and additional components and configurations herein. - The two
cycles condenser 320. The respective flows of therefrigerants condenser 320. The cascade evaporator/condenser 320 may have any suitable size shape, configuration, or capacity. Other components and other configurations may be used herein. - The
refrigerant 200 may be compressed by thehigh side compressors 130 and condensed in thehigh side condenser 150. Therefrigerant 200 may be stored in thehigh side receiver 160 and may be withdrawn as needed to satisfy the load on the cascade evaporator/condenser 320. Therefrigerant 200 then may pass through the suction/liquid heat exchanger 180, the highside expansion device 170 and the cascade evaporator/condenser 320. Therefrigerant 200 again passes through the suction/liquid heat exchanger 180 and returns to thehigh side compressors 130. The suction/liquid heat exchanger 180 may be used to sub-cool therefrigerant 200 before entry into the cascade evaporator/condenser 320. Other components and other configurations may be used herein. - The
low side cycle 120 may be similar. The carbon dioxide based refrigerant 310 may be compressed by thelow side compressors 210 and then pass through the cascade evaporator/condenser 320. The refrigerant 310 may be stored within the low side liquidvapor separator tank 230 and withdrawn as needed. The refrigerant 310 may pass through one or more lowside expansion devices 240 and one or morelow side evaporators 250. Thelow side cycle 120 may be separated into thelow temperature loop 290 and themedium temperature loop 260. Other components and other configurations may be used herein. - The
low side cycle 120 also may use athermosyphon 330. Thethermosyphon 330 provides for the circulation of a fluid, in this case the refrigerant 310, based upon thermal gradients as opposed to mechanical devices such as a pump and the like. In this example, thethermosyphon 330 may have atank inlet 340 in communication with the low side liquidvapor separator tank 230, acompressor inlet 350 in communication with thelow side compressors 210, and acascade outlet 360 in communication with the cascade evaporator-condenser 320. - In use, the liquid/gas flow of the
carbon dioxide refrigerant 310 may be diverted to the low side liquidvapor separator tank 230 where the liquid and vapor may separate therein. The vapor portion may be routed to the cascade evaporator-condenser 320 through thethermosyphon 330 and mixed with the vapor exiting thelow side compressors 210 so as to condense the vapor to a liquid. Other components and other configurations may be used herein. -
FIGS. 1 and 2 show an example of a conventional configuration of thethermosyphon 330. Thecompressor inlet 350 may be in line with thecascade outlet 360. Thetank inlet 340 may merge in a perpendicular relationship at approximately a ninety degree (90°) angle so as to provide thethermosyphon 330 with a substantial tank “T” likeshape 370.FIG. 3 shows a similar configuration in which thetank inlet 340 is in line with thecascade outlet 360 and thecompressor inlet 350 merges perpendicularly for a compressor “T” likeshape 380. In either orientation, the flows merge at about the perpendicular angle. - The flow from the low side liquid
vapor separator tank 230 through thetank inlet 340 may be considered aprimary flow 390. The flow from thecompressors 210 to thecompressor inlet 350 may be considered asecondary flow 400. Given the use of the perpendicular configuration, blocking the respective flows through the pressure dropsensitive thermosyphon 330 may be an operational and an efficiency issue. In a conventional cascade system, theprimary flow 390 through thetank inlet 340 may be at about 435.07 psia (about 3000 kpa) with a temperature of about 22 degrees Fahrenheit (about −5.5 degrees Celsius) and with a mass flow rate of about 0.17 or 0.18 kg/s. Thesecondary flow 400 through thecompressor 360 may be at about 145 degrees Fahrenheit (about 63 degrees Celsius) and with a mass flow rate of about 0.09 kg/s. After merging, amixed outlet flow 410 at thecascade outlet 360 may be at about 434.87 psia (about 2998 kpa), about 45 degrees Fahrenheit (about 7.2 degrees Celsius), and with a mass flow rate of about 0.26 or 0.27 kg/s. Other pressures, temperatures, mass flow rates, and other parameters may be used herein. -
FIG. 4 shows an example of athermosyphon 420 as may be described herein. Thethermosyphon 420 may have atank inlet 430 that is in line with acascade outlet 440. Instead of thecompressor inlet 350 merging into thetank inlet 340 in the perpendicular orientation described above, thethermosyphon 420 may include anangled inlet compressor 450. Theangled compressor inlet 450 may be positioned at an angle θ1 with respect to thetank inlet 430 or the centerline of thecascade outlet 440. The angle θ1 preferably may range from about more than about zero degrees (0°) to about forty-five degrees (45°) or so. Other angles may be used herein. Other components and other configurations may be used herein. -
FIG. 5 shows a further example of athermosyphon 460 as may be described herein. In this example, thethermosyphon 460 may include anangled tank inlet 470 and/or anangled compressor inlet 480. Theinlets cascade outlet 490 for a substantial “Y” like shape. Theangled tank inlet 470 may be positioned at an angle of θ2 with respect to the centerline of thecascade outlet 490. The angle θ2 preferably may range from about more than about zero degrees (0°) to about forty-five degrees (45°) or so. Other angles may be used herein. Theangled compressor inlet 480 also may use the angle θ1 similar to that described above. Specifically, the angles θ1 and θ2 may be the same or different. Other components and other configurations also may be used herein. - The following chart shows the mass flow rate changes with respect to the
thermosyphon 330 ofFIGS. 2 and 3 and thethermosyphons FIGS. 4 and 5 . The comparison assumes the same pressure and temperature at the tank inlet, the same mass flow rate and temperature at the compressor inlet, and the same pressure and temperature at the cascade outlet. The mass flow rate into the tank inlet and out of the cascade outlet will vary. With respect to theangled compressor inlet 450 in thethermosyphon 420 ofFIG. 4 , the angle θ1 was varied from six degrees (6°) to about ninety degrees (90°). Likewise, with respect to theangled tank inlet 470 and theangled compressor inlet 480 of thethermosyphon 460, angle θ1 varied from about ten degrees) (10° to about thirty degrees (30°) and θ2 varied from about three degrees (3°) to about thirty degrees (30°). The respective changes in mass flow rate thus are shown with respect to kilograms per second. -
Angle Compressor Tank Cascade Percent θ1 inlet inlet outlet change FIG. θ1-θ2 (kg/s) (kg/s) (kg/s) from FIG. 2 2 0.09 0.17 0.26 3 0.09 0.18 0.27 5.46 4 6° 0.09 0.24 0.33 41.17 11° 0.09 0.24 0.33 41.17 15° 0.09 0.23 0.32 35.29 30° 0.09 0.23 0.32 35.29 45° 0.09 0.23 0.32 35.29 5 90° 0.09 0.09 0.18 −47.03 10°-10° 0.09 0.22 0.31 29.70 15°-15° 0.09 0.20 0.29 18.29 30°-30° 0.09 0.21 0.30 22.79 14°-3° 0.09 0.22 0.31 32.34 - The tank inlet flow rate and the cascade outlet flow rate thus varied and improved with respect to the perpendicular configuration of
FIGS. 2 and 3 . The use of an angle of about six degrees (6°) to about eleven degrees (11°) improved the mass flow rate at the cascade outlet from about 0.26 kg/s to about 0.33 kg/3 or an increase of about forty-one percent (41%). Varying the angle of thesecondary flow 400 with respect to theprimary flow 390 thus provides an enhanced primary flow rate as compared to the perpendicular angle arrangement and/or a decreased pressure drop along the primary flow for the same inlet velocity. -
FIG. 6 shows a further embodiment of athermosyphon 500 as may be described herein. In this example, thethermosyphon 500 may include atank inlet 510 and aninline cascade outlet 520. In this example, thethermosyphon 500 may include an angled compressor inlet 530. The angle θ1 of the angled compressor inlet 530 thus may vary. The angled compressor inlet 530 may have a variable diameter 540. Likewise, the diameter of the variable diameter 540 may vary. Varying angles and diameters also may be used for thetank inlet 510. Thetank inlet 510 may have a diameter of about 1⅜ inches (about 34.9 millimeters) or so. Other components and other configurations may be used herein. - The following chart shows examples in varying the angle θ1 as well as the diameter from about 0.4 inch (about 10.2 millimeters) to about one (1) inch (about 25.4 millimeters) given the
constant tank inlet 510 described above. -
Compressor Tank Cascade Percent Angle Diameter inlet inlet Outlet change FIG. θ1 (mm) (kg/s) (kg/s) (kg/s) from FIG. 2 6 30° 10.2 0.09 0.35 0.44 106.89 30° 15.2 0.09 0.27 0.36 56.44 30° 20.3 0.09 0.22 0.31 31.27 30° 25.4 0.09 0.22 0.31 27.61 11° 19.1 0.09 0.24 0.33 38.86 - The use of a variable diameter 540 of about 10.2 millimeters with an angle θ1 of about thirty degrees for the angled compressor inlet 530 thus results in more than a 100% improvement over the
FIG. 2 baseline. Specifically, a higher secondary flow from thecompressors 210 may draw more of the refrigerant 310 from the liquidvapor separator tank 230 without obstructing the flow given a jet of a smaller diameter. Likewise, the ratio of the diameters between the angled compressor inlet 530 and the tank inlet varied from about 0.7 to about 0.3 with at least a 0.5 ratio being preferred. - The variable diameter 540 also may be dynamically set depending upon operational parameters. For example, the variable diameter 540 may vary depending upon the load on the overall system and the like. Other parameters may be considered herein. Although the thermosyphons herein have been focused on the use of the
carbon dioxide refrigerant 310, the thermosyphons described herein may be used to merge any type of primary and secondary flows. - It should be apparent that the foregoing relates only to certain embodiments of the present application and the resultant patent. Numerous changes and modifications may be made herein by one of ordinary skill in the art without departing from the general spirit and scope of the invention as defined by the following claims and the equivalents thereof.
Claims (20)
Priority Applications (1)
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US15/007,251 US20160231063A1 (en) | 2015-02-11 | 2016-01-27 | Thermosyphon Configuration for Cascade Refrigeration Systems |
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US201562114603P | 2015-02-11 | 2015-02-11 | |
US15/007,251 US20160231063A1 (en) | 2015-02-11 | 2016-01-27 | Thermosyphon Configuration for Cascade Refrigeration Systems |
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US15/007,251 Abandoned US20160231063A1 (en) | 2015-02-11 | 2016-01-27 | Thermosyphon Configuration for Cascade Refrigeration Systems |
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US (1) | US20160231063A1 (en) |
EP (1) | EP3056838A1 (en) |
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CA (1) | CA2919464A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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US20190301772A1 (en) * | 2018-04-03 | 2019-10-03 | Heatcraft Refrigeration Products Llc | Cooling system |
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Also Published As
Publication number | Publication date |
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EP3056838A1 (en) | 2016-08-17 |
CN105865093A (en) | 2016-08-17 |
CA2919464A1 (en) | 2016-08-11 |
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