期刊文献+

液氢温区直接节流JT制冷机降温实验

Cool-down Experiment of the Direct Throttling JT Cryocooler Working at Liquid Hydrogen Temperature
下载PDF
导出
摘要 空间用大冷量低温制冷机是实现液氢长期在轨零蒸发贮存的关键技术之一。预冷型液氢温区直接节流JT制冷机无低温运动部件,结构简单,降温过程无需旁通,具备实现空间大冷量制冷的潜力,可单独实现冷量远距离传输。采用直接节流流程方案搭建了用GM制冷机预冷的液氢温区直接节流JT制冷机开式系统实验测试平台,阐述了制冷过程,分析了降温过程存在的问题,在20.8 K测得了10.19 W制冷量。 The cryocooler working at liquid hydrogen temperature with a large cooling capacity is one of key technologies for hydrogen zero boil-off storage in space.The precooled direct throttling JT cryocooler has advantages of absence of moving parts at low temperature and simplicity.With the potential to provide a large cooling capacity,it can realize longdistance transmission of cooling capacity separately.Meanwhile,the bypass structure is no longer required during the cooldown process.Based on the scheme of direct throttling JT cryocooler,an open-cycle experimental prototype of the direct throttling JT cryocooler working at liquid hydrogen temperature was built which was precooled by the GM cryocooler.Cool-down process was introduced.The cooling capacity of 10.19 W was measured at 20.8 K.
作者 申运伟 刘东立 刘磊 邱长煦 耑锐 甘智华 SHEN Yunwei;LIU Dongli;LIU Lei;QIU Changxu;ZHUAN Rui;GAN Zhihua(Cryogenics Center,Zhejiang University City College,Hangzhou 310015,China;Key Laboratory of Refrigeration and Cryogenic Technology of Zhejiang Province,Institute of Refrigeration and Cryogenics,Zhejiang University,Hangzhou 310027,China;Key Laboratory of 3D Micro/Nano Fabrication and Characterization of Zhejiang Province,School of Engineering,Westlake University,Hangzhou 310024,China;Shanghai Institute of Aerospace Systems Engineering,Shanghai 201109,China)
出处 《真空与低温》 2022年第3期273-278,共6页 Vacuum and Cryogenics
基金 国家自然科学基金(51806199、61927820) 载人航天预先研究项目(010106)。
关键词 液氢温区 大冷量 直接节流 JT制冷机 liquid hydrogen temperature large cooling capacity direct throttling JT cryocooler
  • 相关文献

参考文献4

二级参考文献83

  • 1Takashi Onaka, Alberto Salama. AKARI: space infrared cooled telescope [ J ]. Exp Astron, 2009, 27:9-17.
  • 2Orlowska A H, Bradshaw T W, Closed cycle coolers for space applications[J]. Space Science Reviews ,1992,61: 233-240.
  • 3Bruce Swinyard, Takao Nakagawa. The space infrared telescope for cosmology and astrophysics: SPICA A joint mission between JAXA and ESA[J]. Exp Astron,2009,23:193-219.
  • 4Glaister D S, Gully W J, Wright G P, et al. A 10 K Cryocooler for Space Applications [ J ]. Cryocoolers, 2001 ( 11 ) :505-511.
  • 5Ross R G Jr. A study of the use of6K ACTDP cryocoolers for the MIRI instrument on JWST[ Jl. Cryocoolers,2004( 13 ) :510-515.
  • 6Glaister D S, Gully W, Ross R G Jr, et al. Aerospace 4-10 K space cryocoolers [ J ], Cryocoolers ,2004 ( 13 ) : 1-7.
  • 7Takao Nakagawa,Keigo Enya,Masayuki Hirabayashi,et al. Fhght Performance of the AKARI Cryogenic System[M]. Publications of the Astronomical Society of Japan,2007.
  • 8Ross R G Jr, Boylet R F, Key R W,et al. NASA advanced cryocooler technology development program [ M ]. International Society of Optical Engineering (SPIE) Conference,2002.
  • 9Scull S R, Jones B G, Bradshaw T W, et al. Design and Development of a 4 K Mechanical Cooler [ J ]. Cryocoolers, 1999 ( 10 ) : 513- 519.
  • 10RADEBAUGH R. Cryocoolers: the state of the art and recent developments[J]. Journal of Physics: Condensed Matter, 2009, 21: 164-219.

共引文献40

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部