期刊文献+

空间有阀无油线性压缩机实验优化 被引量:1

Experimental Optimization of Space Oil-free J-T Compressors
原文传递
导出
摘要 有阀线性压缩机是空间液氦温区节流制冷机的关键部件,为满足液氦温区节流制冷机的需求,基于本实验室研制的动圈式有阀线性压缩机,对两级对置式线性压缩机进行了实验优化。主要针对压缩机的板弹簧特性、输入参数和充气压力等开展相关实验研究,解决压缩机运行过程中出现的活塞中心位置偏移的问题,逐步提升压缩机的性能。最终,在功耗65 W,采用两级级压缩获得了11.8的压比。 Linear JT compressor is one of the key components of the space 4 K JT cryocooler.To fulfill the requirement of the space 4 K JT cooler,experimental optimization is carried out on a two-stage JT linear compressor developed by our laboratory.The characteristics of the plate spring,input power and charge pressure is experimentally studied.The problem of the deviation of piston center position in the operating process of the JT compressor has been solved.And the performance of the two-stage JT compressor is improved.Ultimately,pressure ratio of 11.8 is achieved when the input power is 65 W.
作者 马跃学 王娟 李建国 刘彦杰 梁惊涛 MA Yue-Xue;WANG Juan;LI Jian-Guo;LIU Yan-Jie;LIANG Jing-Tao(Key Laboratory of Space Energy Conversion Technologies,Technical Institute of Physics and Chemistry,Chinese Academy of Sciences,Beijing 100190,China)
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2019年第8期1729-1734,共6页 Journal of Engineering Thermophysics
基金 国家自然科学基金(No.51776213) 国家重点基础研究发展计划(No.613322)
关键词 空间 线性压缩机 优化 压比 space J-T compressor optimization pressure ratio
  • 相关文献

参考文献1

二级参考文献10

  • 1Shinozak K, Sugita H, Sato Y, et al. Developments of 1-4 K class space mechanical coolers for new generation satellite missions in JAXA. In: R G Ross, Jr., ed. Proceedings of the 16th International Cryocooler Conference. Atlanta: Cryocoolers 16, ICC Press, Boulder Colorado, 2010. 1-8.
  • 2Inatani J, Noguchi T, Shi S C, et al. A Submillimeter SIS receiver cooled by a compact stirling-JT refrigerator. In: Blundell R, Tong E,eds. Proceedings of the Eighth International Symposium on Space Terahertz Technology. Cambridge, 1997.273-280.
  • 3Bakos G C, Ioannidis I, Tsagas N F, et al. Experimental and numeri- cal study on a miniature Joule-Thomson cooler for steady-state char- acteristics. Int J Heat Mass Transfer, 2002, 45:609-618.
  • 4Olson J R, Moore M, Champagne P, et al. Development of a space- type 4-stage pulse tube cryocooler for very low temperature. Adv Cryogenic Eng, 2006, 823:623-631.
  • 5Petach M, Durand D, Michaelian M, et al. MIRI cooler system design update. In: R G Ross, Jr., eds. Proceedings of the 16th International Cryocooler Conference. Atlanta: Cryocoolers 16, ICC Press, Boulder Colorado, 2010.9-12.
  • 6Goicoechea J R, Nakagawa T, SPICA team. SPICA: The next generation Infrared Space Telescope. arXiv: 1101.1418 (astro-ph.1M), Accessed 7 Jan 2011.
  • 7Orlowska A H, Bradshaw T W. Closed cycle coolers for space applications. Space Sci Rev, 1992, 61: 233-240.
  • 8Swinyard B, Nakagawa T. The space infrared telescope for cosmol- ogy and astrophysics: SPICA A joint mission between JAXA and ESA. Exp Astron, 2009, 23:193-219.
  • 9Ross R G Jr, Boylet R F, Key R W, et al. NASA advanced cryocooler technology development program. Adv Cryogenic Eng, 2006, 823: 607-614.
  • 10Ross R G Jr. A Study of the use of 6 K ACTDP cryocoolers for the MIRI instrument on JWST. In: R G Ross, Jr., ed. Proceedings of the 13th International Cryocooler Conference. New Orleans Louisian: Cryocoolers 13, ICC Press, Boulder Colorado, 2004. 15-24.

共引文献15

同被引文献3

引证文献1

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