The invention relates to a large battery array for a spacecraft. The large battery array comprises at least one battery assembly (1) and a connecting hinge (2), the battery assembly (1) comprises a substrate (11), a thin film battery array (12) and a fixed connection structure (13). The thin film battery array (12) is arranged on at least one side of the substrate (11); the fixed connection structure (13) is arranged at the edge of the thin film battery array (12) and is used for connecting the substrate (11) and the thin film battery array (12); the fixed connecting structure (13) comprises a connecting rope (131) and threaded connecting pieces (132) arranged on the connecting rope (131) at intervals. Wherein the threaded connecting pieces (132) are arranged at intervals along the edge of the thin film battery array (12) and are used for fixing the position of the thin film battery array (12) on the substrate (11).

    本发明涉及一种用于航天器的大型电池阵,包括:至少一个电池组件(1)和连接铰链(2);所述电池组件(1)包括:基板(11)、薄膜电池阵(12)和固定连接结构(13);在所述薄膜电池阵(12)在所述基板(11)的至少一侧设置;所述固定连接结构(13)设置于所述薄膜电池阵(12)的边缘且用于连接所述基板(11)和薄膜电池阵(12);所述固定连接结构(13)包括:连接绳(131)和在所述连接绳(131)上间隔设置的螺纹连接件(132);其中,所述螺纹连接件(132)沿所述薄膜电池阵(12)的边缘间隔的布置,用于固定所述薄膜电池阵(12)在所述基板(11)上的位置。


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    Titel :

    Large battery array for spacecraft


    Weitere Titelangaben:

    一种用于航天器的大型电池阵


    Beteiligte:
    XIANG JUNHUA (Autor:in) / LI HONGJUN (Autor:in) / YI LUE (Autor:in)

    Erscheinungsdatum :

    06.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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