基于泵变频调速的航天器热控制技术  

Spacecraft Thermal Control Technology Based onVariable Frequency Pump

作　　者：宁献文[1] 张加迅[1] 

机构地区：[1]中国空间技术研究院,北京100094

出　　处：《中国空间科学技术》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

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.

关 键 词：热控制 变频泵 单相流体回路 地面原理样机 航天器 

分 类 号：V448.22[航空宇航科学与技术—飞行器设计]