The invention provides a light-small peripheral novel space docking mechanism, comprising an active docking mechanism and a driven member. The active docking mechanism comprises an active docking frame. The active docking frame is uniformly provided with a plurality of sets of embracing claw mechanisms. The driven member is provided with a plurality of latch handles whose positions are corresponding to positions of the embracing claw mechanisms. The embracing claw mechanisms are respectively used to capture the latch handles on the corresponding positions. The embracing claw mechanism comprises a driving mechanism. The driving mechanism is connected with a driver plate through a bevel gear I and a bevel gear II which are meshed with each other. A driving disk is connected with a center pole. The center pole is connected with a locking claw. The docking mechanism realizes functions of rapid capture and accurate positioning of two aircrafts through locking when the driving mechanisms drive forward and separating when the driving mechanisms drive backward, and finally, functions of docking maintenance and repeated docking of two aircrafts are realized. The mechanism has beneficial effects of compact structure, light weight, reliable capture, and adjustable locking forces, and the mechanism can operate repeatedly.


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    Titel :

    Light-small peripheral novel space docking mechanism


    Beteiligte:
    HOU JIANWEN (Autor:in) / LIU ZHOU (Autor:in) / FU LIJIA (Autor:in) / LIU ZHONG (Autor:in) / ZHENG YUNQING (Autor:in) / SHI ZONGCHENG (Autor:in) / DING TONGCAI (Autor:in) / WANG ZHIYI (Autor:in) / WU YUANBING (Autor:in) / YUAN JIAJIN (Autor:in)

    Erscheinungsdatum :

    16.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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