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空间对接机构结构锁传动原理分析
引用本文:高海波,杨文玉,熊有伦.空间对接机构结构锁传动原理分析[J].上海航天,2001,18(4):15-18.
作者姓名:高海波  杨文玉  熊有伦
作者单位:华中科技大学机械科学与工程学院,
摘    要:针对异体同构周边式对接机构,提出了两种结构锁主动锁钩传动方案,分别对其运动原理及特点进行分析比较。数值仿真结果表明,在不同的电机驱动功率、作动时间和执行端行程等条件下,结构锁传动系统应采用不同传动方案。

关 键 词:对接机构  航天器  结构锁  异体同构  主动锁钩传动方案  传动原理
文章编号:1006-1630(2001)04-0015-04
修稿时间:2000年9月25日

Analysis on the Transmission Principles of Structural Latches of Docking Mechanisms
GAO Hai bo,YANG Wen yu,XIONG You lun.Analysis on the Transmission Principles of Structural Latches of Docking Mechanisms[J].Aerospace Shanghai,2001,18(4):15-18.
Authors:GAO Hai bo  YANG Wen yu  XIONG You lun
Abstract:Structural latches are key components of a docking mechanism. For designing an androgynous peripheral docking mechanism, two transmission models of active structural latches are proposed, and comprehensive comparisons between them are done. Numerical simulation shows that different models should be adopted according to the working conditions, such as engine power, working time and excution end travel.
Keywords:Docking mechanism  Spacecraft  Structural latch  Transmission
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