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超临界氦贮罐实验研究及漏热分析

Experimental research and heat loss analysis of supercritical helium dewar

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【作者】 满满张立强帅彤周浩洋李新宇龚领会徐向东徐冬

【Author】 Man Man1 Zhang Liqiang1 Shuai Tong1 Zhou Haoyang1 Li Xinyu2 Gong Linghui3 Xu Xiangdong3 Xu Dong3(1China Academy of Launch Vehicle Technology Systems Engineering Division,Beijing 100076,China)(2China Academy of Launch Vehicle Technology,Beijing 100076,China)(3State Key Laboratory of Technologies in Space Cryogenic Propellants,Technical Institute of Physics and Chemistry, Chinese Academy of Sciences,Beijing 100190,China)

【机构】 北京宇航系统工程研究所中国运载火箭技术研究院中国科学院理化技术研究所航天低温推进剂技术国家重点实验室

【摘要】 采用高真空多层绝热结构,研制了一套超临界氦球形贮罐。对贮罐进行漏热估算和应力校核,漏热估算为1.44 W,应力符合设计要求。在液氦加注过程中,监测液氦温度波动特别大,且温度计引线管上有结霜现象出现,分析漏热原因是出现了剧烈热声振荡。将温度计引线管与增压管连通,连通后热声振荡消除。对该超临界氦贮罐进行液氦密封憋压绝热性能测试,液氦压力到达2 MPa的时间约7.5 h,压力平均上升速率为0.267 MPa/h,换算成漏热量为12 W,仍远远大于漏热估算值,分析是由于在连通管路中形成了环流,造成较大漏热。提出了该类超临界氦贮罐的设计改进原则。

【Abstract】 A spherical supercritical helium Dewar was developed with high-vacuum multilayer thermal insulation.The heat loss of Dewar was estimated to be 1.44 W and the maximum stress and displacement meet requirements.During the liquid helium filling,the temperature fluctuation in Dewar occurred and the thermometer fairlead was covered with frost,which meant large heat loss.Thermo-acoustic oscillation,may be the reason but disappeared when connecting the thermometer fairlead and pressure inlet.The insulation performance at closed status was measured.The pressure of liquid helium reached 2 MPa for 7.5 h and the rise speed was 0.267 MPa/h.The heat loss was 12 W,which was far larger than the estimated value.The reason may be the circulating flow in the connecting pipe.The design and improvement principles were proposed at last.

【基金】 航天低温推进剂技术国家重点实验室开放研究课题(项目编号SKLTSCP1204)
  • 【分类号】V511
  • 【被引频次】5
  • 【下载频次】180
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