有限空间内活动线束连接器尾夹实施工艺  

Process of Connector Tail Clamp of Movable Harness in Limited Space

作　　者：田景玉[1] 穆希鹏 王玉龙[1] 王威[1] 张伟[1] 张俊[1] Tian Jingyu;Mu Xipeng;Wang Yulong;Wang Wei;Zhang Wei;Zhang Jun(Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033;Shanghai Electro-mechanical Engineering Institute,Shanghai 201109)

机构地区：[1]中国科学院长春光学精密机械与物理研究所,长春130033 [2]上海机电工程研究所,上海201109

出　　处：《航天制造技术》2020年第2期1-3,共3页Aerospace Manufacturing Technology

基　　金：科技部重点研发计划(2018YFB1107303);国家自然科学基金(61535013);吉林省科技发展计划(20190302042GX);装备预研领域基金(61404140107)。

摘　　要：结合某航天项目实际需要,针对活动线束的连接器尾夹处理工艺进行研究,设计了4种工艺方案并测试,确定了在导线间填充环氧胶的工艺方法是一种可靠的压线卡处理工艺,可以确保压紧线束,使活动线束的扰动不对连接点产生应力作用。通过该种工艺实现了某航天产品活动线束的高可靠工艺实施。According to the actual needs of an aerospace project,the connector tail clamp processing technology of the movable wire harness is studied.Four process schemes are designed and tested.It is determined that the process method of filling epoxy glue between wires is a reliable wire clamp processing technology,which can ensure that the wire harness is compressed,so that the disturbance of the movable wire harness does not produce stress effect on the solder joints or crimping joints.Through this process,the high reliable process implementation of the active harness of a aerospace product is realized.

关 键 词：活动线束 连接器尾夹 布线工艺 有限空间 

分 类 号：V46[航空宇航科学与技术—航空宇航制造工程]