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16.1K的高频两级脉冲管制冷机的实验研究 被引量:3

EXPERIMENTAL STUDY OF HIGH FREQUENCY TWO-STAGE PULSE TUBE CRYOCOOLER WITH TEMPERATURE OF 16.1K
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摘要 单级高频脉冲管制冷机直接降低到20 K以下温区存在很大困难,采用多级方案是高频脉冲管制冷机获得更低温度的主要方法。本文介绍了一套高频气耦合型两级脉冲管制冷机的性能特性,该脉冲管制冷机可以达到16.1 K的最低温度,是目前有报道高频气耦合型两级脉冲管制冷机的最低温度。文中给出了双向进气、频率和输入功率对最低温度的影响. Use single stage version to reach the temperature of 20 K is a difficulty for high frequency pulse tube cooler(PTC). Multi-stage version is a popular method to reach the low temperature. This paper introduced the performance of a high frequency gas-couple two-stage PTC, which has reach the lowest temperature of 16.1 K, this is reported lowest temperature for high frequency gas-couple two-stage PTC. The effect of double inlet, frequency and input power on the temperature of cold tip is shown in this paper.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2007年第2期205-207,共3页 Journal of Engineering Thermophysics
基金 国家自然科学基金(No.50206025)
关键词 气耦合 两级 高频脉冲管制冷机 实验 gas-couple two-stage high frequency PTC experiment
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参考文献5

  • 1杨鲁伟,Thummes G.单级高频脉冲管制冷机研究.中国工程热物理学会第十一届年会,北京,2005.
  • 2Olson J R,Kotsubo V,Champagne P J,et al.Performance of a Two-Stage Pulse Tube Cryocooler for Space Applications.Cryocooler 10,New York:KA/PP,1999.163-170.
  • 3Nast TC,Olson J,Evtumov B,et al.Development of a Two-Stage Pulse Tube Cryocooler for 35 K Cooling.Cryocooler 12,New York:KA/PP,2003.213-218.
  • 4Yang Luwei,Thummes G.High Frequency Two-Stage Pulse Tube Cryocooler with Base Temperature Below 20 K.Cryogenics,2005,45:155-159.
  • 5杨鲁伟,Tang Ke,G Thummes.分离型二级高频脉冲管制冷机实验研究.见:第十一届工程热物理年会论文集.北京,2005.632-637.

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同被引文献19

  • 1洪国同,余兴恩,李正宇,杨健慧,李强,李青.超流氦气液相分离器实验装置研制[J].低温工程,2004(3):1-5. 被引量:3
  • 2PUGET J T,NOIT A,CAMUS P.A Closed Cycle Dilution Refrigerator for Space.Presentation at the Novel Approaches to Infrared Astrophysics Workshop[C].Keck Institute for Space Stuidies,2009.
  • 3RINUS C,HENK C,INO W.The Development of The SCIAMCHY Radiant Cooler.Proceeding of the Sixth European Symposium on Space Environmental Control System[C].Noordwijk,Netherlands,20-22 May 1997.
  • 4STEPHEN M V,RUSSELL B.S,BRUCE H.Superfliud Helium Cryostat for the SIRTF Cryogenic Telescope Assembly[J].Proc of SPIE 2003,4850:1038-1049.
  • 5ROSS R G,Jr,JOHNSON D L.NASA's Advanced Cryocooler Technology Development Program (ACTDP)[J].Adv in Cryogenic Engineering.2006,51:607-614.
  • 6DUBANND L,CLERC L,ERCOLANI E.Herschel Flight Models Sorption Coolers[J].Cryogenics,2008,48:95-103.
  • 7SHIRRON PJ,WEGEL D,DIPIRRO MJ.A Continuous Adiabatic Demagnetization Refrigerator for Cooling to 10 mK and Below[J].AIP Conference Proceedings,2006,850:1573- 1581.
  • 8KELLEY R L.The Suzaku High Resolution X-Ray Spectrometer[J].Publ Astron Soc Japan,2007,59:S77-S112.
  • 9TRIQUENEAUX S,SENTIS L,CAMUS P,et al.Design and Performance of the Dilution Cooler System for the Planck Mission[J].Cryogenics,2006,46:288-297.
  • 10Liubiao Chen,Qiang Zhou,Hai Jin,Wenxiu Zhu,Junjie Wang,Yuan Zhou.386<ce:hsp sp="0.25"/>mW/20<ce:hsp sp="0.25"/>K single-stage Stirling-type pulse tube cryocooler[J].Cryogenics.2013

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