The invention relates to a battery assembly, a satellite battery system and a satellite. The battery assembly includes: a battery; the temperature measuring sensor is arranged on the surface of the battery, and the temperature measuring sensor is used for detecting the temperature of the battery; the heating structure is arranged on the long side surface of the battery, and the heating structure is used for heating the battery; the heat insulation structure is arranged on the surface of the battery; and the heat dissipation structure is arranged on the surface of the battery. The battery assembly can be exposed in an external space environment, and normal operation of the satellite is guaranteed.

    本申请涉及一种电池组件、卫星电池系统及卫星。电池组件包括:电池;测温传感器,设置于所述电池的表面,所述测温传感器用于检测所述电池的温度;加热结构,设置于所述电池的长侧面,所述加热结构用于对所述电池进行加热;隔热结构,设置于所述电池的表面;散热结构,设置于所述电池的表面。电池组件能够暴露在外空间环境中,保证卫星正常运行。


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    Title :

    Battery assembly, satellite battery system and satellite


    Additional title:

    一种电池组件、卫星电池系统及卫星


    Contributors:
    QIU SHAOJIE (author) / ZHANG BO (author) / YANG PENG (author) / ZHI JIAYUN (author) / DING TING (author) / LUO SHUN (author) / YANG QIAOLONG (author) / CHANG MING (author)

    Publication date :

    2024-02-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



    Satellite battery testing status

    Haag, R. / Hall, S. | NTRS | 1986


    Satellite battery temperature control

    EDELSTEIN, F. / FLIEGER, H. | AIAA | 1978