电连接器强脱机构测控技术研究  

Research on Measurement and Control Technology of Strong Release Mechanism of Electrical Connector

作　　者：王惠颖[1] 杨佳椿 孟皓 田乙玄 杨继志[1] WANG Hui-Ying;YANG Jia-Chun;MENG Hao;TIAN Yi-Xuan;YANG Ji-Zhi(Beijing Institute of Aerospace Testing Technology,Beijing100074,China)

机构地区：[1]北京航天试验技术研究所,北京100074

出　　处：《机电产品开发与创新》2022年第5期114-116,共3页Development & Innovation of Machinery & Electrical Products

摘　　要：本文介绍了一种飞行器发射前对电连接器进行脱离的强脱机构。文中具体介绍了强脱机构的系统组成、工作原理和测试成效,着重对强脱机构测控技术的设计方案重点阐述。随后又进行了相关的数据测试工作,各项性能指标满足要求,实际应用效果优良。This paper introduces a strong release mechanism for separating the electrical connector before launch. The system composition and working principle of the strong disengagement mechanism are introduced, and it focuses on the design scheme of the measurement and control technology of the strong disengagement mechanism. Then the relevant data test work is carried out, and the performance indexes meet the requirements, and the practical application effect is excellent.

关 键 词：强脱机构 电连接器 测控技术 数据测试 

分 类 号：V44[航空宇航科学与技术—飞行器设计]