一种具有位置反馈功能的航天快速插拔机构及其应用

By designing a spacecraft quick-plug mechanism with position feedback function, the problem of improper insertion during extravehicular operations by astronauts was solved, enabling simple and efficient installation and replacement of electronic equipment, and meeting the operational needs of astronauts.

CN116995489BActive Publication Date: 2026-07-17SOUTHWEST CHINA RES INST OF ELECTRONICS EQUIP

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
SOUTHWEST CHINA RES INST OF ELECTRONICS EQUIP
Filing Date
2023-08-04
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing quick-connect and disconnect mechanisms for aerospace applications suffer from jamming issues during extravehicular operations by astronauts, leading to improper insertion or failure to lock, and thus fail to meet aerospace ergonomic requirements.

Method used

A spacecraft quick insertion and removal mechanism with position feedback function was designed, including a passive end and an active end. The mechanism provides position feedback to ensure proper insertion through the cooperation of a positioning display component and a locking component, and achieves quick locking through the locking component.

Benefits of technology

This allows astronauts to install or replace electronic equipment in one go outside the cabin, avoiding misalignment and repeated operations caused by jamming, and meeting the astronauts' requirements for ease of operation and efficiency.

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Abstract

本发明属于航天机构技术领域,涉及一种具有位置反馈功能的航天快速插拔机构及其应用。一种具有位置反馈功能的航天快速插拔机构,包括配合使用的被动端和主动端;所述被动端侧壁开设有锁紧销孔;所述主动端包括主体结构件、锁紧部件、到位显示部件和到位参考件;所述主体结构件的内腔尺寸与被动端的外形尺寸相匹配;所述到位显示部件和到位参考件配合设置在主体结构件侧壁,用于显示被动端在主体结构件里装插到位或未到位;所述锁紧部件也设置在主体结构件侧壁,用于伸入锁紧销孔,以锁止销定装插在主体结构件里的被动端;或拔出锁紧销孔,以解除对装插在主体结构件里的被动端的锁止销定。操作方便,耗时极短,满足航天员舱外操作工效学要求。
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