›› 2011, Vol. 31 ›› Issue (2): 47-52.doi: 10.3780/j.issn.1000-758X.2011.02.008

• 技术交流 • 上一篇    下一篇

基于泵变频调速的航天器热控制技术

 宁献文, 张加迅   

  1. (中国空间技术研究院,北京 100094)
  • 收稿日期:2010-07-13 修回日期:2010-09-07 出版日期:2011-04-25 发布日期:2011-04-25
  • 作者简介:宁献文 1976年生,2006年获北京航空航天大学人机与环境工程专业博士学位,高级工程师。研究方向为航天器热控制。
  • 基金资助:

    国家863计划

Spacecraft Thermal Control Technology Based onVariable Frequency Pump

 NING  Xian-Wen, ZHANG  Jia-Xun   

  1. (China Academy of Space Technology, Beijing 100094)
  • Received:2010-07-13 Revised:2010-09-07 Online:2011-04-25 Published:2011-04-25

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。

关键词: 热控制, 变频泵, 单相流体回路, 地面原理样机, 航天器

Abstract: 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.

Key words: Thermal control, Variable frequency pump, Single-phase fluid loop , Prototype model , Spacecraft