Analysis of Space Environment Effects and Failure Modes of Aerospace Electrical Connectors

China Mechanical Engineering ›› 2010, Vol. 21 ›› Issue (13): 1598-1604.

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Analysis of Space Environment Effects and Failure Modes of Aerospace Electrical Connectors

Gao Liang1;Chen Wenhua1,2;Liu Juan1;Zhou Shengjun3;Lu Xianbiao3

1.Zhejiang University, Hangzhou, 310027

2.Zhejiang Sci-Tech University, Hangzhou, 310018

3.Hangzhou Aerospace Electrical Technology Co. Ltd, Hangzhou, 310015

Online:2010-07-10 Published:2010-07-15
Supported by:

National Natural Science Foundation of China（No. 50745040);
National High-tech R&D Program of China (863 Program) （No. 2007AA04Z409）

航天电连接器的空间环境效应和失效模式分析

高亮1;陈文华1,2;刘娟1;周升俊3;卢献彪3

1.浙江大学,杭州,310027

2.浙江理工大学,杭州,310018

3.中国航天时代电子公司八二五厂,杭州,310015

基金资助:
国家自然科学基金资助项目(50745040)；国家863高技术研究发展计划资助项目(2007AA04Z409)；民用航天科技预研资助项目(B1220062302)
National Natural Science Foundation of China（No. 50745040);
National High-tech R&D Program of China (863 Program) （No. 2007AA04Z409）

Abstract

Abstract:

Based on the function of electrical connectors in a satellite and the space environment which the electrical connectors confront, a failure mode of the electrical connectors in space environment was analyzed. Firstly, the stress on electrical connectors confronted in orbit was analyzed; then, the effects of the stress on the electrical properties, the sealing properties and the electromagnetic shielding properties and the resulting failure modes were also analyzed. The results show that almost every space environment factor can affect the performance of electrical connector, which leads to electrical connector failures; and that the failure modes of the electrical connectors in space environment are very complex: some of space environment factors may cause a variety of failures, and the competing failure or relevant failure can happen.

Key words: electrical connector, space environment, environment effect, failure mode

摘要：

从卫星对某型电连接器的功能要求和电连接器在轨运行时所面临的空间环境出发,分析了电连接器的空间环境效应和相应的失效模式。首先,分析了电连接器在轨工作时面临的应力;然后,分析了这些应力对电连接器的电性能、密封性能和电磁屏蔽性能的影响,以及由此导致的失效模式。分析表明:几乎每一个空间环境因素都能对电连接器的性能造成影响而导致电连接器失效;电连接器在空间环境综合作用下的失效模式十分复杂,有的空间环境因素会同时导致多种失效,而不同的失效模式之间会形成竞争失效甚至相关失效。

关键词:

电连接器, 空间环境, 环境效应, 失效模式

CLC Number:

TB114.3
V442

GAO Liang, CHEN Wen-Hua, LIU Juan, ZHOU Sheng-Dun, LEI Xian-Biao.

Analysis of Space Environment Effects and Failure Modes of Aerospace Electrical Connectors

[J]. China Mechanical Engineering, 2010, 21(13): 1598-1604.

高亮, 陈文华, 刘娟, 周升俊, 卢献彪.

航天电连接器的空间环境效应和失效模式分析

[J]. 中国机械工程, 2010, 21(13): 1598-1604.

References

[1]黄本诚.黄本诚文集[M].北京:中央编译出版社,2007.
[2]中国科学院空间科学与应用研究中心编.宇航空间环境手册[M],2000:519.
[3]赵伟.航天器微振动环境分析与测量技术发展[J].航天器环境工程,2006(4):210-214.
[4]王浚等著.环境模拟技术[M],1996:764.
[5]高本辉,崔素言著.真空物理[M],1983:617.
[6]化学工业部合成材料老化研究所编.高分子材料老化与防老化[M],1979:435.
[7]刘景军[1],李效玉[1].高分子材料的环境行为与老化机理研究进展[J].高分子通报,2005(3):62-69.
[8]高晓敏[1],何舟[1],杨雪海[1].部分高分子材料老化研究进展[J].合成材料老化与应用,2005,34(1):39-43.
[9]复旦大学高分子科学系编著.高分子化学[M],1995:434.
[10]吴茂英[1].聚合物光老化、光稳定机理与光稳定剂（上）[J].高分子通报,2006(4):76-83.
[11]吴茂英[1].聚合物光老化、光稳定机理与光稳定剂（下）[J].高分子通报,2006(6):89-97.
[12]Gijsman P, Meijers G,Vitarelli G. Comparison of the UV degradation Chemistry of Polypropylene, Poly ethylene, Polyamide 6 and Polybutylene Terephthalate [J].Polymer Degradation and Stability, 1999,65 (3) : 433-441.
[13]尹毅,屠德民.用等温电流法研究自由基清除剂的作用机理：聚合物电老化 …[J].中国电机工程学报,2000,20(3):13-15. 9
[14]张秀阁,胡起宙,田玉珍,任红.高分子聚合物电缆绝缘电树枝老化机理浅析[J].沈阳工程学院学报：自然科学版,1999(4):11-13.
[15]李盛涛,郑晓泉著.聚合物电树枝化[M],2006:205.
[16]Montanari G C. Electrical Life Threshold Modes for Solid Insulating Materials Subjected to Electrical and Multiple Stresses[J]. IEEE Transactions on Electrical Insulation, 1992,27(5) : 974-986.
[17]Montanari G C, Mazzanti G, Simoni L. Progress in Electrothermal Life Modeling of Electrical Insulation during the Last Decades[J].IEEE Transactions on Dielectrics and Electrical Insulation, 2002, 9 (5):730- 744.
[18]冯伟泉[1],丁义刚[1],闫德葵[1],刘学超[1],王伟[1],李冬梅[1].空间电子、质子和紫外综合辐照模拟试验研究[J].航天器环境工程,2005(2):69-72. 5
[19]傅依备.几种高分子材料的核辐射效应研究[J].材料导报,2003,17(2):4-7.
[20]哈鸿飞,吴季兰编著.高分子辐射化学原理与应用[M],2002:219.
[21]姜利祥[1][2],盛磊[1],陈平[1],何世禹[2].环氧树脂648和TDE-85的质子辐照损伤效应研究[J].航天器环境工程,2006(3):134-137.
[22]钟伟 [1],管俊芳 [2],邬博义 [1],陈忍昌 [2].锡须研究的历史与现状[J].电子质量,2005(8):59-63.
[23]王先锋[1],贺岩峰[1].锡须生长机理的研究进展[J].电镀与涂饰,2005,24(8):49-51.
[24]严宗达,王洪礼编著.热应力[M],1993:428.
[25]穆霞英.蠕变力学[M],1990.
[26]WestonDA.电磁兼容原理与应用[M].杨自佑,译.北京:机械工业出版社,2006.
[27]Waterhouse R B.微动磨损与微动疲劳[M].周仲荣,译.成都:西南交通大学出版社,1999:3-10.
[28]王春生,赵熹华.异质金属Fe—Ni电阻点焊熔核形成过程三维数值模拟分析[J].中国机械工程,2000,11(4):449-451.
[29]章继高.大力发展电接触科学—一门重要交叉科学[J].中国机械工程,1999,10(9):966-968.
[30]黄本诚,马有礼著.航天器空间环境试验技术[M],2002:268.
[31]吴正和.浅谈宇航级电连接器的标准和要求[J].机电元件,1999,19(4):51-55.
[32]徐福祥主编.卫星工程概论[M],2004:469.

Analysis of Space Environment Effects and Failure Modes of Aerospace Electrical Connectors

航天电连接器的空间环境效应和失效模式分析

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