The invention provides a satellite cabin plate. The satellite cabin plate comprises a plate body with a containing cavity. The cell structure is positioned in the plate body; the thermal control structure is positioned in the plate body and is used for realizing heat transfer; a multi-curved-surface cell element which is correspondingly matched with the thermal control structure and is used for assisting heat dissipation of the thermal control structure is further arranged in the plate body; the satellite deck further comprises a plurality of connecting structures connected with the cell element structures. And the connecting structure is configured to be used for combining and fixing the plate body and external equipment. The satellite deck is simple in overall structure and convenient to assemble.

    本发明提供一种卫星舱板,包括具有容纳腔的板体;位于板体内的胞元结构;以及位于板体内的用以实现热传递的热控结构;所述板体内还包括与热控结构对应配合的用以辅助热控结构散热的多曲面胞元;所述卫星舱板还包括与胞元结构连接的若干连接结构;所述连接结构被配置为用以将板体与外部设备结合固定。该卫星舱板整体结构简单,且装配方便。


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    Titel :

    Satellite deck


    Weitere Titelangaben:

    一种卫星舱板


    Beteiligte:
    LI WEI (Autor:in) / XIAO DENGBAO (Autor:in) / XING CHUNYING (Autor:in) / MA TIECHANG (Autor:in) / SHI LIANG (Autor:in)

    Erscheinungsdatum :

    2023-04-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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