期刊文献+

基于泵变频调速的航天器热控制技术 被引量:8

Spacecraft Thermal Control Technology Based onVariable Frequency Pump
下载PDF
导出
摘要 文章针对某单相流体回路地面原理样机,提出采用泵变频调速技术进行控温,并对系统控温特性进行了地面试验研究,整个瞬态试验过程中控温精度一般都在±0.3℃以内,最大波动也基本不超过±0.5℃,基于泵变频调速技术的热控制策略性能优良、有效,试验结果可供实际工程设计参考。 The traditional temperature control mode using temperature-sensing valve has three deficiencies with the reliability,dynamic behavior,pump operational efficiency.In order to solve these problems,a new thermal control technology based on variable frequency pump was put forward for a fluid loop prototype model.The temperature control performance of the thermal control technology based on variable frequency pump was tested.During all transients,the controlled temperature was within the range of ±0.3℃ around the set-point,with a maximum admissible variation range of ±0.5℃.Thermal control strategy based on variable frequency pump has effective performance.
出处 《中国空间科学技术》 EI CSCD 北大核心 2011年第2期47-52,共6页 Chinese Space Science and Technology
基金 国家863计划(2009AA7044008)资助项目
关键词 热控制 变频泵 单相流体回路 地面原理样机 航天器 Thermal control Variable frequency pump Single-phase fluid loop Prototype model Spacecraft
  • 相关文献

参考文献8

  • 1DAVID G GILMORE. Spacecrafl thermal control handbook [M]. 2nd ed. The Aerospace Press, El Segundo, California, 2002.
  • 2姜军 徐济厅.载人航天器液体冷却回路系统性能.载人航天,2004,(2).
  • 3范含林.神舟飞船热设计及飞行温度数据分析[J].航天器工程,2003,12(1):31-35. 被引量:6
  • 4范含林,黄家荣,刘庆志,张立.载人运输飞船流体回路方案研究[J].中国空间科学技术,2007,27(5):38-43. 被引量:13
  • 5MATTHIJSSEN R, VAN PUT P, VANDERI.1ST M C A M. Development of an advanced mechanically pumped fluid loop for thermal control of large future telecomunication platforms [R]. Bradford Engineering B. V., 2007.
  • 6PRADEEP BHANDARI, GAJANANA C BIRUR. Long lerm life testing of a mechanically pumped cooled loop for spacecrafl thermal control [R]. AIAA-97-2/170, AIAA ThermophysicsConference, Atlanta, GA, 1997.
  • 7曹显锋,马桂庆.变频技术在风机、水泵上的应用[J].天津冶金,2009(4):47-49. 被引量:1
  • 8KatsuhikoOgata 著 卢伯英 于海勋 译.现代控制工程[M].北京:电子工业出版社,2000..

二级参考文献3

  • 1黄俊 王兆安.电力电子变流技术[M].北京:机械工业出版社,1999..
  • 2范含林.神舟飞船热设计及飞行温度数据分析[C].空间飞行器总体专业委员会年会,2002.
  • 3PATEL V P, BARIDO RICHARD, et al. Development of the Internal Thermal Control System (ITCS) for International Space Station (ISS) [C]. 31st International Conference on Environmental Systems, 2002.

共引文献21

同被引文献96

引证文献8

二级引证文献33

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部