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.
作者
王惠颖
杨佳椿
孟皓
田乙玄
杨继志
WANG Hui-Ying;YANG Jia-Chun;MENG Hao;TIAN Yi-Xuan;YANG Ji-Zhi(Beijing Institute of Aerospace Testing Technology,Beijing100074,China)
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
关键词
强脱机构
电连接器
测控技术
数据测试
Strong release mechanism
Electrical connector
Measurement and control technology
Data test