The invention provides a flexible overclothes for a spacecraft, the flexible overclothes is used for covering a final assembly test platform so as to store the spacecraft, the final assembly test platform is provided with a top surface, a base, an opening side, a stair side and two side walls, and the flexible overclothes is modularly designed. Comprising a first module covering the base, a third module and a sixth module covering the two side walls respectively, a fifth module covering the stair side, and a second module matched with an opening formed by the top face and the opening side in shape and used for covering the opening part. Wherein the modules forming the flexible overclothes are connected with one another in a matched mode and cover the whole general assembly test platform, and the second module is a movable module and can be folded and unfolded. By means of the flexible vesture, the effects of high fitting degree and high operation efficiency can be achieved.

    本发明提供了一种航天器用柔性罩衣,用于覆盖总装测试平台,从而贮存航天器,所述总装测试平台具有顶面、底座、开口侧、楼梯侧以及两个侧壁,所述柔性罩衣为模块化设计,包括覆盖所述底座的第一模块、分别覆盖所述两个侧壁的第三模块和第六模块、覆盖楼梯侧的第五模块、与顶面和开口侧形成的开口形状配合,用于覆盖开口部分的第二模块;其中,组成所述柔性罩衣的各模块之间相互配合连接,覆盖整个总装测试平台,所述第二模块为活动模块,可以收拢和展开。采用本发明的柔性罩衣,能够实现贴合度高,作业效率高的效果。


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    Title :

    Flexible overclothes for spacecraft


    Additional title:

    一种航天器用柔性罩衣


    Contributors:
    TIAN SHUAI (author) / LIU JINGSONG (author) / SUI YUNLIANG (author) / LIU ZHENG (author) / QI QIANG (author) / PEI YANXUE (author) / ZHANG JIANHUI (author) / YANG CHANGXI (author) / LI XIAOFANG (author) / PAN LULU (author)

    Publication date :

    2023-10-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS





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