郭元东, 周强, 刘欣彤, 等. 35 K深低温制冷与热传输集成系统研究[J]. 真空与低温, 2022, 28(3): 353-358. DOI: 10.3969/j.issn.1006-7086.2022.03.016
引用本文: 郭元东, 周强, 刘欣彤, 等. 35 K深低温制冷与热传输集成系统研究[J]. 真空与低温, 2022, 28(3): 353-358. DOI: 10.3969/j.issn.1006-7086.2022.03.016
GUO Yuandong, ZHOU Qiang, LIU Xintong, et al. Research on 35 K Cryogenic Refrigeration and Heat Transfer Integrated System[J]. VACUUM AND CRYOGENICS, 2022, 28(3): 353-358. DOI: 10.3969/j.issn.1006-7086.2022.03.016
Citation: GUO Yuandong, ZHOU Qiang, LIU Xintong, et al. Research on 35 K Cryogenic Refrigeration and Heat Transfer Integrated System[J]. VACUUM AND CRYOGENICS, 2022, 28(3): 353-358. DOI: 10.3969/j.issn.1006-7086.2022.03.016

35 K深低温制冷与热传输集成系统研究

Research on 35 K Cryogenic Refrigeration and Heat Transfer Integrated System

  • 摘要: 深低温系统在天文观测和深空探测等空间应用中具有重要作用。降低制冷温度有利于提高探测系统的测量精度,获得较高的信噪比。设计研制一种基于脉冲管制冷机(PTC)和深冷环路热管(CLHP)的集成系统,连接部分采用一体式耦合设计,消除了系统安装界面,减小了界面热阻。采用两台35 K脉冲管制冷机,分别作为两套35 K氖工质深冷环路热管的热沉,热管蒸发器可以为同一个探测器耦合,实现系统的备份冗余设计。为了减小周围环境的寄生漏热,设计了低温铜质冷屏,冷屏热沉采用80 K脉冲管制冷机。集成系统的环路热管可以实现约2 W的热量传输,最大传输距离510 mm,为我国未来深空探测技术提供了技术支持。

     

    Abstract: Cryogenic systems play an important role in space applications such as astronomical devices and deep space exploration.Lowering the refrigeration temperature can improve the measurement accuracy of the detection system,thereby obtaining a higher signal-to-noise ratio.An integrated system based on pulse tube cooler and cryogenic loop heat pipe is designed and manufactured.The integrated connection design is adopted and the installation interface is omitted.Two 35 K pulse tube coolers are used as heat sinks for two sets of 35 K neon cryogenic loop heat pipes.The heat pipe evaporators can be coupled to the same detector to realize the backup redundancy design of the system.A low-temperature heat-insulating cold shield is designed to reduce the parasitic heat leakage in the surrounding environment,and the 80 K pulse tube refrigerator is used as the cold shield heat sink.The loop heat pipe of the integrated system can realize the heat transmission of about 2 W,with a maximum transmission distance of 510 mm,which provides technical support for future deep space exploration technology.

     

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