CIESC Journal ›› 2025, Vol. 76 ›› Issue (S1): 114-122.DOI: 10.11949/0438-1157.20241296

• Fluid dynamics and transport phenomena • Previous Articles    

Development and testing of an independent two-stage valved linear compressor for space applications

Xinquan SHA1(), Ran HU1,2, Lei DING1(), Zhenhua JIANG1,2, Yinong WU1,2   

  1. 1.Shanghai Institute of Technical Physics, Chinese Academy of Sciences, Shanghai 200083, China
    2.University of Chinese Academy of Sciences, Beijing 100049, China
  • Received:2024-11-13 Revised:2024-11-25 Online:2025-06-26 Published:2025-06-25
  • Contact: Lei DING

空间用单机两级有阀线性压缩机研制及测试

沙鑫权1(), 胡然1,2, 丁磊1(), 蒋珍华1,2, 吴亦农1,2   

  1. 1.中国科学院上海技术物理研究所,上海 200083
    2.中国科学院大学,北京 100049
  • 通讯作者: 丁磊
  • 作者简介:沙鑫权(1994—),男,硕士研究生,助理工程师,18817656275@163.com
  • 基金资助:
    中国科学院率先行动“引才计划”人才项目;国家自然科学基金项目(51806231);中国科学院战略性先导科技专项(B类)(XDB35000000);JZX7Y20220414101801

Abstract:

In cosmic exploration, a dependable low-temperature environment is indispensable for space detectors. The valved linear compressor (VLC) functions as the core component in the Joule-Thomson (JT) throttling cryocooler, with its structure and performance having a direct bearing on the cryocooler's cooling efficacy and efficiency. To attain lightweight and efficient VLCs for space applications, the motion characteristics of the double-acting piston structure are analyzed, building on the research foundation of our group. The gas load is then determined using the describing function method. By optimizing the motor structure and gas valve, an independent two-stage VLC prototype is developed, accompanied by variable parameter studies across different charging pressures and piston strokes. Experimental findings reveal that as the charging pressure rises from 0.1 MPa to 0.3 MPa, the mass flow rate increases by 337%, while the pressure ratio decreases by just 19.7%. Both motor efficiency and isentropic efficiency peak at 0.15 MPa. As the piston stroke expands from 2 mm to 10 mm, the mass flow rate multiplies by 10.6, and the pressure ratio increases by 9.6 times. Motor efficiency peaks at 4 mm, whereas isentropic efficiency demonstrates a linear increase with stroke length. Testing confirms that this compressor's maximum output performance is 16 mg/s at a pressure ratio of 19.7, sufficient to match the output capacity of two single-stage compressors. The creation of this prototype establishes a foundation for meeting the lightweight and efficient demands of future space throttling cryocoolers.

Key words: compressor, non-linear load, gas valve, optimization, output capacity, experimental validation, lightweight and efficient

摘要:

在宇宙探索中,可靠的低温环境对空间探测器至关重要。有阀线性压缩机是Joule-Thomson(JT)节流制冷机的驱动部件,其结构及性能直接影响制冷机制冷性能及效率。基于课题组研究基础,本文优化压缩机电机及气阀,研制了一款单机两级有阀线性压缩机原理样机并开展相关研究测试。实验结果表明,随着充气压力从0.1 MPa增加至0.3 MPa时,质量流量增长337%,压比仅降低19.7%,电机效率与等熵效率在0.15 MPa时达到最大;随着活塞行程从2 mm增加至10 mm时,质量流量增长了10.6倍,压比增长了9.6倍,电机效率在4 mm时达到最大,而等熵效率与行程呈线性增长趋势。该压缩机最大输出性能为16 mg/s(19.7压比),能覆盖两台单级压缩机的输出能力。该原理样机的研制,为后续空间节流制冷机的轻量高效需求奠定了基础。

关键词: 压缩机, 非线性负载, 气阀, 优化, 输出能力, 实验验证, 轻量高效

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