SU1312348A1 - Cryogenic unit ejector stage - Google Patents
Cryogenic unit ejector stage Download PDFInfo
- Publication number
- SU1312348A1 SU1312348A1 SU853946039A SU3946039A SU1312348A1 SU 1312348 A1 SU1312348 A1 SU 1312348A1 SU 853946039 A SU853946039 A SU 853946039A SU 3946039 A SU3946039 A SU 3946039A SU 1312348 A1 SU1312348 A1 SU 1312348A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- ejector
- cooling
- evaporator
- cryogenic
- zones
- Prior art date
Links
- 238000001816 cooling Methods 0.000 claims abstract 9
- 239000007788 liquid Substances 0.000 claims abstract 4
- 238000004519 manufacturing process Methods 0.000 claims 1
- 238000005057 refrigeration Methods 0.000 abstract description 2
- 238000009434 installation Methods 0.000 abstract 3
- 238000009835 boiling Methods 0.000 abstract 1
- 239000003795 chemical substances by application Substances 0.000 abstract 1
- 238000010586 diagram Methods 0.000 abstract 1
- 230000004907 flux Effects 0.000 abstract 1
- 238000005086 pumping Methods 0.000 abstract 1
- 239000003507 refrigerant Substances 0.000 abstract 1
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
- 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
Abstract
Изобретение относитс к области криогенного машиностроени Целью изобретени вл етс повьшение экономичности при охлаждении пр мым потоком при сверхкритическом давлении Изобретение относитс к холодильной технике, а точнее к криогенным гелеевым установкамо Целью изобретени вл етс повышение экономичности при охлаждении пр мым потоком при сверхкритическом давлении и наличии прот женных магистралей в объекте охлаждени о На чертеже представлена схемй эжекторной ступени Эжекторна ступень содержит испаритель 1, переохладитель 2, дрост сель 3, линии 4 и 5 пр мого и обратного потоков, теплообменники 6 и 7, объект 8 охлаждени , эжектор 9, Предложенна установка работает следующим образомо Газовый пр мой поток предварительно охлажденного криогента при сверхи наличии прот женных магистралей в объекте охлаждени . Поставленна цель достигаетс тем, что в эжекторной ступени криогенной установки, содержащей испаритель 1 и предохранитель 2, первые зоны которых подключены к линии 5 обратного потока, а жидкостные зоны сообщены посредством дроссел 3j теплообменники 6 и 7 и эжектор 9, вход которого подключен к линии 4 пр мого потока, а выход и камера смешени - к первым зонам, объект 8 озслаждени включен в лш-и1ю 4 пр мого потока через эжектор 9, что позвол ет обеспечить заданные услови криостатировани при меньших расходах хладагента о 1 ил с критическом давлении по линии 4 проходит последовательно через теплообменники 6 и 7, отдава свое тепло кип щей жидкости, и поступает в объект 8 охлаждени о В объекте 8 крио- гент воспринимает тепловую нг.грузку, вследствие чего его температура повьг- шаетс и направл етс далее в активное сопло эжектора 9 о Кинетическа энерги расшир ющегос потока исполь-. зуетс в эжекторе дл создани разрежени и понижени температуры в переохладителе 2 путем откачки из нее паров Благодар тому, что активное . сопло э ;ектора 9 установлено на выходе газообразного криогента из объекта 8, заданные услови криостатиро- ва1ш объекта с высоким тепловым потоком и прот женными гидравлическими сх tOBU. ю со 4 00The invention relates to the field of cryogenic engineering. The aim of the invention is to increase the economy when cooling with direct flow at supercritical pressure. The invention relates to refrigeration equipment, and more specifically to cryogenic gel installations. The purpose of the invention is to increase the economy with cooling with direct flow at supercritical pressure and long lines in the cooling facility. The drawing shows the ejector stage diagram. The ejector stage contains evaporator 1, subcooled itel 2, drost sel 3, lines 4 and 5 of direct and reverse flow, heat exchangers 6 and 7, cooling facility 8, ejector 9, the proposed installation works as follows: Gas pre-cooled cryogent direct flow with super-high lines in the cooling facility . The goal is achieved by the fact that in the ejector stage of a cryogenic installation containing an evaporator 1 and a fuse 2, the first zones of which are connected to the line 5 of the reverse flow, and the liquid zones are communicated through droplets 3j, heat exchangers 6 and 7 and ejector 9, whose input is connected to line 4 direct flow, and the output and mixing chamber to the first zones, the cooling object 8 is included in the first 4 direct flow through the ejector 9, which allows to ensure the specified conditions of cryostatisation with less refrigerant costs m pressure through line 4 passes successively through heat exchangers 6 and 7, giving up its heat to the boiling liquid, and enters the cooling object 8 About object 8, the cryogen agent perceives thermal ng load, as a result of which its temperature goes down and is directed further into the active nozzle of the ejector 9 o Kinetic energy of the expanding flow is used - is ejected in the ejector to create a vacuum and lower the temperature in subcooler 2 by pumping vapors out of it, thanks to being active. the nozzle e; vector 9 is installed at the exit of the gaseous cryogenic from the object 8, defined by the conditions of the cryostatting of the object with a high heat flux and extended hydraulic systems. y co 4 00
Description
магистрал ми достигаетс при меиьших расходах пр мого потока через рефрижераторную установкуhighways are achieved at the lowest direct flow through the refrigeration unit
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU853946039A SU1312348A1 (en) | 1985-08-19 | 1985-08-19 | Cryogenic unit ejector stage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU853946039A SU1312348A1 (en) | 1985-08-19 | 1985-08-19 | Cryogenic unit ejector stage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU1312348A1 true SU1312348A1 (en) | 1987-05-23 |
Family
ID=21194818
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU853946039A SU1312348A1 (en) | 1985-08-19 | 1985-08-19 | Cryogenic unit ejector stage |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU1312348A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120285661A1 (en) * | 2011-01-14 | 2012-11-15 | Caitin, Inc. | Vapor absorption system |
| US8887525B2 (en) | 2009-09-04 | 2014-11-18 | Pax Scientific, Inc. | Heat exchange and cooling systems |
| CN104481725A (en) * | 2014-11-13 | 2015-04-01 | 西安航空动力股份有限公司 | Self-pressurization method and device for hydrogen or helium |
-
1985
- 1985-08-19 SU SU853946039A patent/SU1312348A1/en active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8887525B2 (en) | 2009-09-04 | 2014-11-18 | Pax Scientific, Inc. | Heat exchange and cooling systems |
| US20120285661A1 (en) * | 2011-01-14 | 2012-11-15 | Caitin, Inc. | Vapor absorption system |
| CN104481725A (en) * | 2014-11-13 | 2015-04-01 | 西安航空动力股份有限公司 | Self-pressurization method and device for hydrogen or helium |
| CN104481725B (en) * | 2014-11-13 | 2016-01-13 | 西安航空动力股份有限公司 | A kind of working medium be hydrogen or helium from boosting method and device |
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