The invention relates to the field of satellites, in particular to a flexible solar wing adjusting device which is mounted on a satellite body and comprises a bearing plate, the bearing plate is arranged at one end of the satellite body, overturning plates are rotationally connected to the two sides of the bearing plate, and rotating plates are rotationally connected to the sides, away from the bearing plate, of the overturning plates; a solar wing is arranged on the side, deviating from the overturning plate, of the rotating plate, a first driving part for driving the solar wing to be unfolded or folded is further arranged on the rotating plate, and a rotating assembly for driving the rotating plate to rotate and an overturning assembly for driving the overturning plate to rotate are arranged on the bearing plate. The solar wing has the effect of improving the reliability and flexibility of rotation of the solar wing.

    本申请涉及卫星的领域,尤其是涉及一种柔性太阳翼调节装置,其安装于卫星本体上,包括承载板,所述承载板设置于卫星本体的一端,所述承载板的两侧均转动连接有翻转板,所述翻转板背离承载板的一侧转动连接有旋转板,所述旋转板背离翻转板的一侧设置有太阳翼,所述旋转板上还设置有驱使太阳翼展开或收拢的第一驱动件,所述承载板上设置有驱使旋转板转动的转动组件和驱使翻转板转动的翻转组件。本申请具有提高太阳翼转动的可靠性和灵活性的效果。


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    Title :

    Flexible solar wing adjusting device and satellite


    Additional title:

    一种柔性太阳翼调节装置及卫星


    Contributors:
    XU MING (author) / ZHANG GUOHONG (author) / WU YONGQING (author) / XU ZHI (author) / ZHU ZHENGXIAN (author) / LUO ZHIHUI (author)

    Publication date :

    2024-02-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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