The invention provides a solar cell array driving mechanism, one end of the solar cell array driving mechanism is connected with a solar cell array, the other end of the solar cell array driving mechanism is connected with an energy storage system and a control system, the solar cell array driving mechanism comprises a rotating part and a fixing part, the fixing part sleeves the rotating part, and a gap space is reserved between the fixing part and the rotating part; the fixed part is provided with a rotating end electric connector at one end of the solar cell array, and is provided with a fixed end electric connector at the other end; a flexible printed board is arranged in a gap space between the rotating part and the fixed part, and the two ends of the flexible printed board are connected with the rotating end electric connector and the fixed end electric connector respectively.

    本发明提供了一种太阳电池阵驱动机构,一端连接太阳电池阵,另一端连接储能系统和控制系统,包括:旋转部件和固定部件,所述固定部件套设在所述旋转部件的外部,所述固定部件和所述旋转部件之间预留有缝隙空间;所述固定部件在太阳电池阵一端设置有转动端电连接器,另一端设置有固定端电连接器;所述旋转部件和固定部件之间的缝隙空间中设置有柔性印制板,所述柔性印制板的两端分别与所述转动端电连接器和所述固定端电连接器连接。


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    Titel :

    Solar cell array driving mechanism


    Weitere Titelangaben:

    一种太阳电池阵驱动机构


    Beteiligte:
    WANG TONG (Autor:in) / JING GUIRU (Autor:in) / YU HAOHUA (Autor:in) / ZHU JIAHAO (Autor:in) / LI WEI (Autor:in) / WANG XUEQIANG (Autor:in) / MORITO (Autor:in) / XU JUNHENG (Autor:in) / WANG YUAN (Autor:in)

    Erscheinungsdatum :

    2022-12-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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