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基于双四杆机构的可重复自动锁紧解锁装置

黄大兴 蒋秋香 张凯 姜景明 杨德财 王治易 钱志源

上海航天(中英文)2023,Vol.40Issue(6):18-23,53,7.
上海航天(中英文)2023,Vol.40Issue(6):18-23,53,7.DOI:10.19328/j.cnki.2096-8655.2023.06.003

基于双四杆机构的可重复自动锁紧解锁装置

A Repetitive Automatic Locking/Unlocking Device Based on Double Four-Bar Mechanism

黄大兴 1蒋秋香 1张凯 1姜景明 1杨德财 1王治易 2钱志源2

作者信息

  • 1. 上海宇航系统工程研究所,上海 201109
  • 2. 上海宇航系统工程研究所,上海 201109||上海市空间飞行器机构重点实验室,上海 201109
  • 折叠

摘要

Abstract

In view of the in-orbit multiple locking/unlocking requirements for the solar alpha rotary joints of the Mengtian lab module under docking and transposition conditions,a repetitive automatic locking/unlocking device is designed,where the double four-bar mechanism and the adaptive end effector are applied.In order to validate the function and performance of the locking/unlocking device,the developed product is tested in various states such as vacuum high-temperature,vacuum low-temperature,and atmospheric environment.The results show that the product can realize the repetitive automatic locking/unlocking function in various states.When the rated direct current operating voltage is 28 V,the execution time of the locking action is between 17.09 s and 17.15 s,and the execution time of the unlocking action is between 16.51 s and 16.89 s.The device has the advantages such as high reliability,full angle,and repetitive locking/unlocking in orbit,and has great engineering application potential in the locking/unlocking mechanisms for spacecrafts.

关键词

对日定向转动关节/锁紧解锁/全角度/可重复/在轨

Key words

solar alpha rotary joint/locking/unlocking/full angle/repetitive/in orbit

分类

航空航天

引用本文复制引用

黄大兴,蒋秋香,张凯,姜景明,杨德财,王治易,钱志源..基于双四杆机构的可重复自动锁紧解锁装置[J].上海航天(中英文),2023,40(6):18-23,53,7.

上海航天(中英文)

OACSCDCSTPCD

2096-8655

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