The invention relates to the technical field of satellite assembly, in particular to a satellite general assembly support vehicle which comprises a support, a turnover platform and a rotation driving part, the turnover platform is pivoted to the top end of the support through a rotating shaft extending in the horizontal direction, and the rotation driving part is installed on the support and used for driving the turnover platform to rotate. The rotation driving part is used for driving the overturning platform to rotate relative to the support, the rotation driving part is used for limiting the position of the overturning platform relative to the support, and the overturning platform is used for being connected with a satellite. The invention aims to provide a satellite general assembly support vehicle aiming at at least one technical problem related in the background technology.

    本申请涉及卫星装配技术领域,具体而言,涉及一种卫星总装支架车,包括支架、翻转平台和转动驱动件,所述翻转平台通过在水平方向上延伸的转轴枢接于所述支架的顶端,所述转动驱动件安装于所述支架,所述转动驱动件用于带动所述翻转平台相对所述支架转动,且所述转动驱动件用于限定所述翻转平台相对所述支架的位置,所述翻转平台用于与卫星连接。本申请的目的在于针对背景技术中所涉及的至少一个技术问题,提供一种卫星总装支架车。


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    Titel :

    Satellite general assembly support vehicle


    Weitere Titelangaben:

    卫星总装支架车


    Beteiligte:
    HUANG HONGZHOU (Autor:in) / ZHANG YABIN (Autor:in) / CHANG ZHENGYONG (Autor:in) / MENG YINAN (Autor:in) / SUI YUANYUAN (Autor:in) / WANG YUNING (Autor:in) / ZHANG SHASHA (Autor:in)

    Erscheinungsdatum :

    20.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B66F HOISTING, LIFTING, HAULING, OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD , Hub-, Verhol- oder Schubvorrichtungen, soweit nicht anderweitig vorgesehen, z.B. Vorrichtungen mit unmittelbarer Krafteinwirkung auf die Last



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