The invention provides a small space docking mechanism for action time sequence decoupling, and belongs to the field of spacecraft space on-orbit service. The mechanism comprises a server side and a target side, a large-angle tolerance guiding docking process is carried out by utilizing an edge molded surface, and a space cam mechanism is adopted to complete the plugging process of an electric connector. An electromechanical heating integrated docking design scheme for realizing mechanical locking and then electric connector plugging under large docking tolerance is provided for the small space docking mechanism, so the problem of realizing action time sequence decoupling under the condition of not occupying extra resources is solved, and the docking reliability is improved from the designsource. The small space docking mechanism is simple and compact in design, small in occupied space and large in guide tolerance.

    本发明提供一种动作时序解耦的小型空间对接机构,属于航天器空间在轨服务领域。该机构包括服务端和目标端,利用边缘型面进行大角度容差的导向对接过程,采用空间凸轮机构完成电连接器的插拔过程,为小型空间对接机构提供了在大对接容差下实现“先机械锁紧后电连接器插接”的机电热一体化对接设计方案,解决了在不占用额外资源的情况下实现动作时序解耦的问题,从设计根源上提高了对接可靠性,本发明设计简单紧凑,占用空间小,导向容差大。


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    Title :

    Small space docking mechanism for action time sequence decoupling


    Additional title:

    一种动作时序解耦的小型空间对接机构


    Contributors:
    KONG NING (author) / ZHUANG YUAN (author) / WANG YAOBING (author) / MA SHUAI (author) / REN JIE (author) / LI LIN (author) / ZHANG JIE (author) / WANG BO (author) / WANG WENLONG (author) / LIU WEI (author)

    Publication date :

    2020-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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