The invention discloses a satellite solar panel back heat dissipation system, which comprises a coupling plate and a heat conduction path, and is characterized in that the coupling plate comprises a satellite solar panel and a radiation plate, and the radiation plate is coupled to the back of the satellite solar panel; the heat conduction channel is communicated with the radiant panel and heat consumption equipment installed on a satellite. According to the heat dissipation system, the heat dissipation advantage condition of the back face of the solar panel is fully utilized, the radiant panel is coupled to the back face of the solar panel to form an integrated coupling plate, the heat dissipation capacity of a high-heat-consumption satellite can be greatly improved, and a guarantee is provided for the satellite to carry multiple loads; and the arrangement of the radiation plate and the heat conduction path in the heat dissipation system does not change the original structure arrangement of the satellite, so that the problem that the heat dissipation system interferes other structures on the satellite is avoided, and the normal operation of the satellite is ensured.

    本发明公开了一种卫星太阳帆板背面散热系统,包括:耦合板和导热通路,所述耦合板包括卫星太阳帆板和辐射板,所述辐射板耦合在所述卫星太阳帆板的背面;所述导热通路连通所述辐射板和安装在卫星上的热耗设备。该散热系统充分的利用太阳帆板背面具有的散热优势条件,将辐射板耦合在太阳帆板的背面做成一体化的耦合板,不仅能够极大的提高高热耗卫星的散热能力,为卫星搭载多载荷提供保障,而且散热系统中的辐射板和导热通路的设置未改变卫星的原有结构设置,不会造成散热系统对卫星上其他结构的干扰问题,保证了卫星的正常运转。


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    Titel :

    Satellite solar panel back heat dissipation system


    Weitere Titelangaben:

    一种卫星太阳帆板背面散热系统


    Beteiligte:
    CHEN ZEGUI (Autor:in) / WANG LEI (Autor:in) / ZHANG TAO (Autor:in)

    Erscheinungsdatum :

    01.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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