US3557566A - Method and device for producing cold and liquefying gases - Google Patents
Method and device for producing cold and liquefying gases Download PDFInfo
- Publication number
- US3557566A US3557566A US743668A US3557566DA US3557566A US 3557566 A US3557566 A US 3557566A US 743668 A US743668 A US 743668A US 3557566D A US3557566D A US 3557566DA US 3557566 A US3557566 A US 3557566A
- Authority
- US
- United States
- Prior art keywords
- medium
- pressure
- enthalpy
- reservoir
- temperature
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title abstract description 18
- 239000007789 gas Substances 0.000 title description 12
- 238000010586 diagram Methods 0.000 abstract description 10
- 230000008569 process Effects 0.000 abstract description 4
- 238000005057 refrigeration Methods 0.000 abstract description 4
- 239000001307 helium Substances 0.000 description 13
- 229910052734 helium Inorganic materials 0.000 description 13
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 12
- 238000010438 heat treatment Methods 0.000 description 10
- 230000001105 regulatory effect Effects 0.000 description 7
- 238000001816 cooling Methods 0.000 description 6
- 239000007788 liquid Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Images
Classifications
-
- 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
- F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
- F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
- F25J1/02—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
- F25J1/0243—Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
- F25J1/0257—Construction and layout of liquefaction equipments, e.g. valves, machines
- F25J1/0275—Construction and layout of liquefaction equipments, e.g. valves, machines adapted for special use of the liquefaction unit, e.g. portable or transportable devices
- F25J1/0276—Laboratory or other miniature devices
-
- 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
- F25B9/08—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using ejectors
-
- 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
- F25B2341/00—Details of ejectors not being used as compression device; Details of flow restrictors or expansion valves
- F25B2341/001—Ejectors not being used as compression device
- F25B2341/0012—Ejectors with the cooled primary flow at high pressure
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S62/00—Refrigeration
- Y10S62/902—Apparatus
- Y10S62/91—Expander
Definitions
- JACOBUS A.VAN DEN BORN INVENTOR JAN HAISMA FERDINAND J.M KROON AGENT Jam. 26, '1971 J. A. VAN DEN BORN ET L METHOD AND DEVICE FOR PRODUOING COLD AND LIQUEFYING GASES Filed July 10, 1968 2 Sheets-Sheet 2 JACOBUS A.VAN DEN BORN INVENTOR) JAN S FERDINAND J;.-M.KROON ZMA GENT "United States Patent 01 ice US. Cl.
- ABSTRACT OF THE DISCLOSURE A process of producing refrigeration and liquefying gasses in which the gas is compressed and refrigerated, to have specific enthalpy, before expansion through a jet ejector, that corresponds to the enthalpy associated with the constant enthalpy line substantially tangent to the boundary line of the liquid-vapour region in the temperature-enthrophy diagram of the medium.
- the gas after passing through the ejector is collected in a high-pressure reservoir which communicates through a throttling valve with the vapor space in the low pressure reservoir.
- the invention relates to a method for producing cold and for liquefying gases, in which a high-pressure medium is cooled below its inversion temperature associated with the relevant pressure and is then supplied to the jet nozzle of at least one ejector; the suction side of the ejector is connected to a minimum pressure reservoir which then communicates through a choking cock to a further reservoir, an outlet duct of the further reservoir communicates with the ejector outlet.
- the invention furthermore relates to a device suitable for carrying out this method.
- ejector is to denote a device in which the potential energy of a high-pressure (primary) medium is converted wholly or partly into kinetic energy, which is utilized at least partly for raising the pressure of a secondary medium.
- the energy of the high-pressure medium supplied to the ejector is utilized at least partly for drawing off the vapour from the minimum pressure reservoir and to raise this pressure to the value prevailing in the outlet. Consequently, in the minimum pressure reservoir a lower pressure and hence a lower temperature will prevail than in the outlet. The cold is therefore supplied at a lower temperature than that corresponding to the pressure of the medium in the outlet.
- the compression ratio may be comparatively low.
- the method and the device according to the invention are particularly suitable for producing cold at very low temperatures, with which very low vapour pressures are associated.
- a particular phenomenon in this case is that in the ejector, not only a reduction of pressure of the primary medium owing to the Joule-Kelvin effect, but also a compression of the secondary medium are obtained.
- the need for cold at temperatures below 4 K. is constantly increasing, particularly for cooling devices such as supraconductive coils and cryogenic computer or storage elements of electronic computers. With these temperatures are associated, as stated above, very low vapour 3,557,566 Patented Jan.
- the suction pressure obtainable at a minimum with an ejector is determined by the speed with which the medium leaves the jet nozzle. Therefore, an ultrasonic structure of the jet nozzle is necessary for attaining these low suction pressures.
- the invention has for its object to provide a method and a device of the kind set forth, in which owing to the lower suction pressure of the ejector obtainable cold can be supplied at lower temperatures than has hitherto been possible.
- the method according to the invention is characterized in that the temperature and the pressure of the cooled high-pressure medium prior to entering the jet nozzle are chosen so that the enthalpy of the medium corresponds with the enthalpy associated with the line of constant enthalpy which is at least approximately tangential to the boundary line of the liquid-vapour region in the temperature-entropy diagram of the medium concerned.
- the temperature and the pressure of the high-pressure medium, prior to entering the jet nozzle are chosen so that the entropy of this medium is lower than the entropy associated with its critical point.
- the invention furtermore relates to a device suitable for carrying out said method, which device comprises a high-pressure medium supply communicating through one or more heat exchangers, in which this medium is cooled below its inversion temperature associated with said pressure to a jet nozzle of one or more ejectors; the suction side of each ejector communicates with a low-pressure reservoir which communicates through a choking cock and, optionally through a further reservoir, to an outlet duct. The outlet of the ejector also communicates through such further reservoir to the outlet duct.
- This device is characterized in that after the last heat exchanger the supply duct is in thermal contact with the medium in the ejector outlet or in the further reservoir, while the device comprises further means for adjusting the temperature of the high-pressure medium prior to entry in the jet nozzle so that at the prevailing pressure the temperature of the high-pressure medium prior to entry in the jet nozzle is such that the enthalpy of the medium corresponds substantially with the enthalpy associated with the line of constant enthalpy which is at least approximately tangential to the boundary line of the liquid-vapour region in the temperature-entropy diagram of the medium concerned.
- a device which is capable of producing, due to the very low suction pressure of the ejector, cold at very low temperatures.
- the means for adjusting the desired temperature of the medium prior to its entry in the jet nozzle is formed by a controllable heating member, which is in thermal contact with that portion of the supply duct which is located between the jet nozzle and the area where the supply duct is in thermal contact with the ejector outlet or the further reservoir.
- a controllable heating member By means of this controllable heating member the temperature can be regulated so that the enthalpy of the medium invariably corresponds with said value.
- the heating member may be formed by an electrical incandescent helix or a thermally conductive connection (copper strip) between the cold part of the supply duct and an area of higher temperature.
- the means for the adjustment of the desired temperature is formed by a circulation duct communicating (a) at one end with the supply duct at an area located between (i) the last heat exchanger and (ii) the area where the supply duct is in contact with the ejector outlet or the further reservoir, and (b) at the other end again with the supply duct just before the jet nozzle, said circulation duct being in thermal contact with a heating member by which heat can be supplied to the medium, the device comprising one or more control-cocks by which the portion of the high-pressure medium flow passing through the circulation duct can be regulated.
- a further advantageous embodiment is characterized in that there is provided a circulation duct which communicates (a) at one end with the supply duct at an area located in front of the outlet side of said medium leaving the last heat exchanger, viewed in the direction of flow of the high-pressure medium, and (b) at the other end with the supply duct just in front of the jet nozzle, said device comprising one or more control-cocks by which the por tion of the high-pressure medium flow passing through the circulation duct can be regulated. In this way the temperature can be adjusted to the desired value.
- FIG. 1 shows diagrammatically and not to scale a device for producing cold at low temperatures.
- FIG. 2 shows diagrammatically and not to scale a temperature-entropy diagram.
- reference numeral 1 designates a compressor.
- the outlet 2 of this compressor communicates with a heat exchanger 3, where the compressed high-pressure medium is in thermal contact with expanded lowpressure medium flowing to the inlet 4.
- the compressed medium in the heat exchanger 5 is in thermal contact with a cold-gas refrigerator 6, shown diagrammatically.
- the high-pressure medium is then in the heat exchanger 7 in thermal contact with expanded medium.
- the medium is further cooled by a cold-gas refrigerator 9, after which in the heat exchanger 10 the medium is again in thermal contact with expanded medium.
- the outlet of the last heat exchanger 10 communicates with a stream dividing cock 11.
- This dividing cock communicate two ducts 12 and 13, which joint at the area 14, where they communicate in common with the jet nozzle 15 of the ejector 16.
- the diffusor 17 of the ejector 16 communicates with a duct 18, which opens out in a reservoir 19.
- the vapour space of the reservoir 19 communicates through a duct 20 and the low-pressure sides of the heat exchangers 10, 7 and 3 with the inlet valve 4 of the compressor 1.
- the reservoir 19 communicates through the duct 21 including a choking cock 22 with the minimum pressure reservoir 23.
- the vapour space of the minimum pressure reservoir 23 communicates openly with the suction side 24 of the ejector 16.
- the duct 13 is in thermal contact at 25 with the medium in the reservoir 19, and the duct 12 is in thermal contact with the heating member 26.
- This device Helium is compressed in the compressor 1 to about atm. and then cooled in the heat exchangers 3, 5, 7, 8, and 10.
- the dividing cock 11 the supplied How of helium is divided into a portion passing through the duct 13 in contact with liquid helium under atmospheric pressure, and a portion passing through the duct 12 in contact with the heating member 26.
- the two portions of the stream are remixed at 14.
- the cock 11 divides the stream so that at the area 14 the medium has an enthalpy corresponding with the enthalpy associated with the isenthalpy tangential to the boundary line of the liquid-vapour region.
- the boundary line of the liquid-vapour region is indicated by 30 and the tangential isenthalpy by 31 in the T5. diagram.
- the pressure of the medium is 30 atm.
- the temperature at the area 14 has to be T In this case the point 33', determined by 12:30 atm. and T is just located on the isenthalpy curve 31, which is tangential to the liquid-vapour region.
- the pressure is lower, for example, 20 atm., because a smaller circulating mass stream is desired, the dividing cock 11 has to be adjusted so that a larger mass stream passes through the duct 12.
- the temperature at the area 14 will thus increase until the enthalpy corresponds with the enthalpy of point 34'. It is then ensured that the initial conditions are such that the entropy value of the medium prior to its entry in the ejector is lower than the entropy value associated with the critical point 35'. In this way a very satisfactory suction effect is always obtained.
- the suction pressure may be a factor 10 lower than in devices in which the medium stream is cooled prior to entry in the jet nozzle to the utmost, that is to say to about 4 K.
- a pressure of 10 mm. Hg can be maintained in the reservoir 23, which corresponds to a temperature of K.
- the helium supplied to the jet nozzle 15 expands therein and at the end of the jet nozzle, owing to its ultrasonic shape, the
- .- helium will have a very high speed and a low pressure.
- the diffusor 17 the pressure of the medium together with the vapour sucked out of the reservoir 23 increases to about 1 atmosphere and then flows through the duct 18 to the reservoir 19. From the reservoir 19 vapour flows through the outlet 20 and said heat exchangers to the inlet of the compressor. A further portion of the medium of the reservoir 19 is supplied via the choking cock 22, where the pressure is reduced, to the reservoir 23. In this way a device is obtained which permits of obtaining cold at very low temperatures in the reservoir 23.
- FIG. 3 shows schematically a device corresponding largely with that of FIG. 1.
- the adjustment of the desired temperature at the area 14 is obtained in this case by the whole high-pressure helium stream being in thermal contact in the heat exchanger 25 with the liquid helium in the reservoir 19, after which the whole helium stream is in thermal contact with a controllable heating member 30.
- a quantity of heat can be supplied to the high-pressure helium stream, and the temperature at the area 14 is such that the enthalpy again corresponds with the value of the isenthalpy curve 31 of the diagram of FIG. 2 for the prevailing pressure.
- F IG. 4 shows schematically an arrangement corresponding with the arrangements of FIGS. 1 and 3.
- a circulation duct 32 which communicates at one end at the area 33 through a controlcock 34 with the high-pressure helium supply duct.
- the area 33 is located, viewed in the direction of fiow of the high-pressure medium, in front of the outlet side of the last heat exchanger 10.
- the circulation duct 32 communicates at the area 14 with the high-pressure medium supply duct.
- connection of the circulation duct 32 at the area 33 with the supply duct is chosen only by Way of example. If desired, the connection may be established farther upstream for example at the area 40 or farther downstream, for example, at the area 41.
- a method of producing cold and liquifying gases including cooling a high-pressure medium to below its inversion temperature associated with the relevant pressure, and then expanding said medium through a jet nozzle of an ejector the suction side of which communicates with a minimum pressure reservoir which in turn communicates through a throttling valve to a further reservoir communicating in turn with the ejector outlet, comprising the further steps of controlling the temperature and the pressure of the cooled high-pressure medium prior to its entry in the jet nozzle, such that the enthalpy of the medium approximately corresponds to the enthalpy associated with the constant enthalpy line which is at least substantially tangent to the boundary line of the liquid-vapour region in the temperature-entropy diagram of the medium concerned.
- a method according to claim 1 comprising the further step, prior to entry of the medium into the jet nozzle,
- a method according to claim 1 comprising the further steps: prior to entry of the medium into the jet nozzle, separating the flow of the medium into two streams and heating one stream to a temperature higher than the other, subsequetnly joining the streams, with their temperatures controlled as required to achieve the appropriate temperature for said selected enthalpy.
- a method according to claim 1 comprising the further step of controlling the temperature and the pressure of the high-pressure medium prior to its entry into the jet nozzle, such that the entropy of this medium is lower than the entropy associated with the critical point of said medium.
- a device for refrigerating and liquifying gases including a high-pressure medium supply, at least one refrigeration means for cooling the medium to below its inversion temperature, an ejector nozzle including (i) an inlet for receiving the medium from the heat exchanger, (ii) an outlet, and (iii) a suction side for expansion of the medium, a low-pressure reservoir communicating with said suction side, a throttling valve, and a further reservoir communicating (i) with the low-pressure reservoir via the throttling valve, (ii) with the nozzle outlet, and (iii) with said high-pressure source, regulating means for adjusting the temperature of the highpressure medium prior to its entry in the jet nozzle, so that at the prevailing pressure, the temperature of said medium is such that its enthalpy corresponds substantially to the enthalpy associated with the line of constant enthalpy which is at least substantially tangential to the boundary line of the liquid-vapour region in the tempera ture-entropy diagram of the
- a device controls the temperature and the pressure of the high-pressure medium prior to its entry in the jet nozzle such that the entropy of this medium is lower than the entropy associated with the critical point of said meduim.
- a device further comprising a supply duct for transporting medium from the source through the refrigerator means and through the high-pressure reservoir for further cooling the medium to the nozzle inlet, the regulating means providing heat to said supply duct and medium therein immediately prior to its entry of the nozzle.
- a device further comprising a supply duct for transporting medium from the source through the refrigeration means and through the highpressure reservoir for futher cooling the medium, and an auxiliary duct inter-connecting said nozzle and supply duct while by-passing the high-pressure reservoir, and valve means for selectively flowing medium from the medium supply through the supply and auxiliary ducts, whereby some of the medium from the supply duct is transportable via the auxiliary duct to the nozzle in a less-cooled state.
- a device further comprising means for heating the medium in the auxiliary duct.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Clinical Laboratory Science (AREA)
- Jet Pumps And Other Pumps (AREA)
- Separation By Low-Temperature Treatments (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL6710358A NL6710358A (es) | 1967-07-27 | 1967-07-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3557566A true US3557566A (en) | 1971-01-26 |
Family
ID=19800807
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US743668A Expired - Lifetime US3557566A (en) | 1967-07-27 | 1968-07-10 | Method and device for producing cold and liquefying gases |
Country Status (8)
Country | Link |
---|---|
US (1) | US3557566A (es) |
AT (1) | AT283291B (es) |
BE (1) | BE718597A (es) |
CH (1) | CH489765A (es) |
FR (1) | FR1573734A (es) |
GB (1) | GB1230419A (es) |
NL (1) | NL6710358A (es) |
SE (1) | SE333385B (es) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3828564A (en) * | 1970-02-27 | 1974-08-13 | Linde Ag | Closed refrigerant cycle for the liquefaction of low-boiling gases |
US4474592A (en) * | 1982-10-20 | 1984-10-02 | Sulzer Brothers Ltd. | Apparatus for producing liquid para-hydrogen |
US20090232665A1 (en) * | 2008-03-12 | 2009-09-17 | Denso Corporation | Ejector |
CN101762110B (zh) * | 2010-02-06 | 2012-09-12 | 大连理工大学 | 共容腔散热式气波制冷机 |
CN104315741A (zh) * | 2014-09-30 | 2015-01-28 | 河南科技大学 | 混合工质喷射式制冷循环系统及制冷循环方法 |
EP1589301B1 (en) * | 2000-03-15 | 2017-06-14 | Denso Corporation | Ejector cycle system with critical refrigerant pressure |
CN110953751A (zh) * | 2018-12-24 | 2020-04-03 | 李华玉 | 第一类热驱动压缩式热泵 |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107560316A (zh) * | 2016-06-30 | 2018-01-09 | 通用电气公司 | 天然气液化系统和方法 |
FR3108740B1 (fr) * | 2020-03-25 | 2022-08-12 | Absolut System | Système de régulation de la température d’un fluide cryogénique |
EP4116639A1 (de) * | 2021-07-05 | 2023-01-11 | Linde Kryotechnik AG | Vorkühlkreis und verfahren zur helium-kälteversorgung |
-
1967
- 1967-07-27 NL NL6710358A patent/NL6710358A/xx unknown
-
1968
- 1968-07-10 US US743668A patent/US3557566A/en not_active Expired - Lifetime
- 1968-07-24 SE SE10081/68A patent/SE333385B/xx unknown
- 1968-07-24 CH CH1109768A patent/CH489765A/de not_active IP Right Cessation
- 1968-07-24 GB GB1230419D patent/GB1230419A/en not_active Expired
- 1968-07-25 BE BE718597D patent/BE718597A/xx unknown
- 1968-07-26 AT AT727468A patent/AT283291B/de not_active IP Right Cessation
- 1968-07-26 FR FR1573734D patent/FR1573734A/fr not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3828564A (en) * | 1970-02-27 | 1974-08-13 | Linde Ag | Closed refrigerant cycle for the liquefaction of low-boiling gases |
US4474592A (en) * | 1982-10-20 | 1984-10-02 | Sulzer Brothers Ltd. | Apparatus for producing liquid para-hydrogen |
EP1589301B1 (en) * | 2000-03-15 | 2017-06-14 | Denso Corporation | Ejector cycle system with critical refrigerant pressure |
EP1134517B1 (en) * | 2000-03-15 | 2017-07-26 | Denso Corporation | Ejector cycle system with critical refrigerant pressure |
US20090232665A1 (en) * | 2008-03-12 | 2009-09-17 | Denso Corporation | Ejector |
CN101762110B (zh) * | 2010-02-06 | 2012-09-12 | 大连理工大学 | 共容腔散热式气波制冷机 |
CN104315741A (zh) * | 2014-09-30 | 2015-01-28 | 河南科技大学 | 混合工质喷射式制冷循环系统及制冷循环方法 |
CN110953751A (zh) * | 2018-12-24 | 2020-04-03 | 李华玉 | 第一类热驱动压缩式热泵 |
Also Published As
Publication number | Publication date |
---|---|
SE333385B (es) | 1971-03-15 |
CH489765A (de) | 1970-04-30 |
AT283291B (de) | 1970-07-27 |
FR1573734A (es) | 1969-07-04 |
NL6710358A (es) | 1969-01-29 |
DE1751665B2 (de) | 1976-05-20 |
BE718597A (es) | 1969-01-27 |
GB1230419A (es) | 1971-05-05 |
DE1751665A1 (de) | 1971-08-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3277660A (en) | Multiple-phase ejector refrigeration system | |
US11448432B2 (en) | Adaptive trans-critical CO2 cooling system | |
US3150498A (en) | Method and apparatus for defrosting refrigeration systems | |
US2522787A (en) | Method of and apparatus for liquefying gases | |
US4242885A (en) | Apparatus for a refrigeration circuit | |
US3300991A (en) | Thermal reset liquid level control system for the liquefaction of low boiling gases | |
CN108626902A (zh) | 用于高环境温度的具有增强的过冷的跨临界系统 | |
US3557566A (en) | Method and device for producing cold and liquefying gases | |
US3368364A (en) | Refrigeration control system | |
US4123914A (en) | Energy saving change of phase refrigeration system | |
US3442093A (en) | Apparatus and ejector for producing cold | |
US4346563A (en) | Super critical helium refrigeration process and apparatus | |
US3735601A (en) | Low temperature refrigeration system | |
US20240302081A1 (en) | Pre-cooling circuit and method for supplying helium refrigeration | |
JPH1163686A (ja) | 冷却サイクル | |
KR940000732B1 (ko) | 영구가스 스트림(stream) 액화방법 | |
US3199304A (en) | Methods for producing low temperature refrigeration | |
US3932158A (en) | System for cooling an object with coolant cycle | |
US3456456A (en) | Cryogenic apparatus for producing cold | |
US2195228A (en) | Refrigerating apparatus and process | |
US3307370A (en) | Cooling device for helium | |
GB1435773A (en) | Refrigeration process and plant having an incorporated cascade circuit and a precooling circuit | |
US5265426A (en) | Compression circuit for a low pressure low temperature gaseous fluid | |
US6170290B1 (en) | Refrigeration process and plant using a thermal cycle of a fluid having a low boiling point | |
US3252291A (en) | Cryo-pumps |