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大型空间展开机构常压高低温环境模拟试验系统研制
引用本文:张良俊,吴静怡,黄永华,徐世超,刘祎石,徐烈.大型空间展开机构常压高低温环境模拟试验系统研制[J].航天器环境工程,2016,33(4):428-433.
作者姓名:张良俊  吴静怡  黄永华  徐世超  刘祎石  徐烈
作者单位: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 上海市空间飞行器机构重点实验室, 上海 201108
基金项目:国家重大科技专项载人航天、探月工程及高分研制保障条件统筹建设项目;上海市科学技术委员会资助项目(编号:06dz22105)
摘    要:为各类大型空间展开机构地面可靠性验证试验提供高低温环境,研制了一种常压高低温环境模拟试验系统。该系统的保温箱体结构采用内、外框架的结构形式,内、外框架之间的连接采用绝热玻璃纤维增强复合塑料杆,其目的是:在进行大温差高低温交变环境试验时,有助于结构的热边界条件稳定;合理的气流组织布局设计有助于内部高低温环境的快速建立,使温度分布更加均匀;冷热源供给系统可稳定地提供高低温环境建立所需冷量及热量;干燥氮气置换系统可实现高低温环境下的超低露点温度;基于PLC的测控系统对试验系统进行高精度测量及控制。试验表明,此大型空间展开机构常压高低温环境模拟试验系统能满足型号产品试验过程中对温度范围、变温速率、温度场均匀性及露点温度的要求。

关 键 词:空间展开机构  温度环境模拟  气流组织  露点温度  试验验证
收稿时间:2016/2/24 0:00:00
修稿时间:8/9/2016 12:00:00 AM

Design and experiment of an innovative simulation system for thermal environment with normal atmosphere pressure used for large-scale space deployable mechanism testing
ZHANG Liangjun,WU Jingyi,HUANG Yonghu,XU Shichao,LIU Yishi,XU Lie.Design and experiment of an innovative simulation system for thermal environment with normal atmosphere pressure used for large-scale space deployable mechanism testing[J].Spacecraft Environment Engineering,2016,33(4):428-433.
Authors:ZHANG Liangjun  WU Jingyi  HUANG Yonghu  XU Shichao  LIU Yishi  XU Lie
Institution:1. Institute of Refrigeration and Cryogenics, Shanghai Jiao Tong University, Shanghai 200240, China;2. Shanghai Key Laboratory of Spacecraft Mechanism, Aerospace System Engineering Shanghai, Shanghai 201108, China
Abstract:An innovative Thermal Environmental Simulation System (TESS) of reliability demonstration for testing large-scale space deployable mechanisms is developed and investigated experimentally. While maintaining the stable thermal boundary conditions, the TESS''s insulation chamber structure can adapt to a large temperature difference between the high and the low temperature environments, with two independent inner and outer frameworks connected by insulating glass fiber reinforced plastics in key nodes. A reasonable airflow distribution design ensures an excellent temperature uniformity of high and low temperature environments. The stable heat and cold source supply system can provide enough energy to achieve the target thermal environment. The dry nitrogen replacement system is established to obtain an ultra-low dew point temperature. The measurement and control system based on the PLC is adopted. Experimental results show that the temperature range, the temperature change rate, the temperature uniformity and the dew point of the TESS can meet the testing requirements totally and admirably.
Keywords:space deployable mechanism  thermal environment simulation  airflow distribution  dew point temperature  experiment validation
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