结合TEC的泵驱两相温控系统的空间应用
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  • 英文篇名:Space Applications of Pumped Two-Phase Temperature Control System Combined with TEC
  • 作者:王镇锐 ; 张兴斌 ; 温世喆 ; 何振辉
  • 英文作者:WANG Zhen-rui;ZHANG Xing-bin;WEN Shi-zhe;HE Zhen-hui;School of Physics,Sun Yat-Sen University;School of Physics and Astronomy,Sun Yat-Sen University;State Key Laboratory of Optoelectronic Materials and Technologies,Sun Yat-Sen University;
  • 关键词:半导体制冷片 ; 泵驱两相回路 ; 平行流换热器 ; R134a
  • 英文关键词:Thermoelectric cooling chip;;Pumped two-phase loop;;Parallel flow heat exchanger;;R134a
  • 中文刊名:YHXB
  • 英文刊名:Journal of Astronautics
  • 机构:中山大学物理学院;中山大学物理与天文学院;中山大学光电材料与技术国家重点实验室;
  • 出版日期:2018-10-30
  • 出版单位:宇航学报
  • 年:2018
  • 期:v.39
  • 基金:两相系统实验平台关键技术研究项目(TZYY08001);; 中山大学珠海市重点实验室空间技术中心项目(71000-42080001)
  • 语种:中文;
  • 页:YHXB201810014
  • 页数:9
  • CN:10
  • ISSN:11-2053/V
  • 分类号:121-129
摘要
为满足天舟一号货运飞船(TZ1)蒸发冷凝科学实验的控温需求,采用半导体制冷片(TEC)和泵驱两相回路结合的控温系统实现了冷凝台-5~40℃(±0. 2℃)的控温要求。对TEC和平行流换热器进行了研究,结果表明该系统能够满足环境温度等于30℃工况下的制冷和散热要求。测试结果表明,平行流换热器在地面和在轨的换热相当,说明重力的影响几乎可以忽略。
        In order to meet the requirements of the evaporation and condensation experiments in Tianzhou-1 cargo spaceship(T Z-1),the system combining the thermoelectric cooling chip(TEC) with the pumped two-phase loop has realized the condensation stage temperature control requirement of-5-40 ℃(± 0. 2 ℃). The research on T EC and the parallel flow heat exchanger shows that the system can meet the requirements of the cooling and heat dissipation under the condition of the ambient temperature equal to 30 ℃. The results show that the heat transfer of the parallel flow heat exchanger on the ground and on orbit is comparable,indicating that the effect of gravity is almost negligible.
引文
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