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单相流体回路工质的试验研究 被引量:2

Experimental Research of Working Fluid Used in Single-Phase Fluid Loop System
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摘要 介绍了单相流体回路设计中流体工质的基本性能参数与选择标准,还介绍了流体回路试验平台;比较了"神舟"飞船流体工质和混合物Secool-3工质的物理特性参数,并进行了室温工况和低温工况试验,试验结果表明Secool-3工质应用于单相流体回路具有较好的系统性能。 Selecting working fluid is an important content of designing single-phase fluid loop system. The chief parameters and criterions for selecting working fluid were considered. The test platform of single-phase fluid loop system was introduced. Based on comparing the chief parameters between the fluid used for Shen Zhou spacecraft and Secool-3 which is one kind of mixture, the experiments at room temperature and low temperature were carried on. The result of the experiments indicates that the single-phase fluid loop system has good performance when Secool-3 mixture is applied.
出处 《中国空间科学技术》 EI CSCD 北大核心 2009年第1期45-51,共7页 Chinese Space Science and Technology
关键词 单相流体回路 流体工质 热控制 试验研究 航天器 Single-phase fluid loop system Work fluid Thermal control Experimental research Spacecraft
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  • 1Felix Berner,Marcel Schleicher,Ledford O C. Fluid Loop System for Use in Spacecraft Thermal Control. ASME E-24147, 1977. 被引量:1

共引文献13

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  • 1张立,范含林.单相流体回路系统的性能集成分析[J].中国空间科学技术,2004,24(4):47-53. 被引量:14
  • 2刘庆志,刘炳清,钟奇.与流体回路耦合的空间辐射器流动/传热分析[J].航天器工程,2007,16(3):65-68. 被引量:9
  • 3Maynard R S. Fluidic momentum controller: U. S., 4, 776, 541. 1988-10-11. 被引量:1
  • 4Wyatt T W, Swet C J. Combined fluid flywheel and pro- pulsion system for spaeecraft: U.S., 3, 862, 732. 1975- 01-28. 被引量:1
  • 5Rasmusson J K. Self contained rotator apparatus: US, 4, 662, 178. 1987-05-05. 被引量:1
  • 6Lurie B J, Schie J A, Iskenderian T C. Fluid loop reaction system: U.S., 5, 026, 008. 1991-06-25. 被引量:1
  • 7Iskenderian T C. Liquid angular-momentum compensator. NASA Tech Briefs, 1989, 13(5): 80. 被引量:1
  • 8Lurie B J, Schier J A. Liquid-ring attitude-control system for spacecraft. NASA Tech Briefs, 1990, 14(9): 82. 被引量:1
  • 9张世杰,曹喜滨,单晓微,等.航天器热控制和液体动量轮一体化执行机构:中国,200910091063.2010-0127. 被引量:1
  • 10Kelly A, McChesney C, Smith P, et al. A performance test of a fluidic momentum controller in three axes. Final Report ASE 463Q, Department of Aerospace Engineering Mechanics, The University of Texas at Austin, 2004. 被引量:1

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