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热负荷对R141b热力学排气系统自增压特性及排气损失的影响

陈忠灿 黄永华 汪彬 李鹏 孙培杰 王天祥 崔佳勋

化工学报2016,Vol.67Issue(10):4047-4054,8.
化工学报2016,Vol.67Issue(10):4047-4054,8.DOI:10.11949/j.issn.0438-1157.20160613

热负荷对R141b热力学排气系统自增压特性及排气损失的影响

Effect on self-pressurization characteristics and mass loss of thermodynamic vent system for refrigerant R141b by heat load

陈忠灿 1黄永华 1汪彬 1李鹏 2孙培杰 2王天祥 3崔佳勋1

作者信息

  • 1. 上海交通大学制冷与低温工程研究所,上海 200240
  • 2. 上海宇航系统工程研究所,上海 201108
  • 3. 航天低温推进剂技术国家重点实验室,北京 100028
  • 折叠

摘要

Abstract

In order to study the fundamental problems involved in the storage of cryogens in space, the experimental investigation of tank pressure control was carried out on a simulator of thermodynamic vent system (TVS), which works at room temperature with refrigerant R141b as working fluid. The pressure control characteristics were obtained at heat load of 120, 160 and 200 W. The test results showed that the self-pressurization rate were 6.43, 12.92 and 18.05 kPa·h−1 respectively at those three different heat load. Mass loss as a result of tank pressure control was compared between TVS method and direct gas vent method. Taking the heat load of 120 W as an example, the mass loss can be reduced by 79.3%. Assuming the mixture vented directly at zero-gravity containing 40% liquid, the TVS method can reduce the mass loss even by up to 84.7%. It was proved that the TVS method cannot only control the tank pressure but also significantly reduce the loss of the storage fluid.

关键词

R141b/热力学/压力控制/传热/相变

Key words

R141b/thermodynamics/pressure control/heat transfer/phase change

分类

航空航天

引用本文复制引用

陈忠灿,黄永华,汪彬,李鹏,孙培杰,王天祥,崔佳勋..热负荷对R141b热力学排气系统自增压特性及排气损失的影响[J].化工学报,2016,67(10):4047-4054,8.

基金项目

航天低温推进剂技术国家重点实验室基金项目(SKLTSCP1206-W)。@@@@Foundation item:supported by the Open Research Fund of the State Key Laboratory of Technologies in Space Cryogenic Propellants (SKLTSCP1206-W) (SKLTSCP1206-W)

化工学报

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