The invention relates to the technical field of frame panel type satellites, and provides a main frame of a frame panel type satellite, which is characterized by comprising a frame comprising a plurality of rod pieces; and a connecting member connecting the frames. The modular and standardized design concept is adopted, single and standardized rod pieces and connecting parts are used, and the modular and standardized rod pieces can be used for constructing main frames of different satellite platforms within 1 ton or used for load cabins of large satellites with larger weight, so that the design cost and the manufacturing cost of the satellites can be greatly reduced, and the design cost and the manufacturing cost of the satellites are greatly reduced. Therefore, a foundation is laid for batch production, standardization and low cost of a satellite platform. According to the technical scheme, the cost of the main frame of the satellite can be reduced by at least 80%, and good economic benefits are achieved.

    本发明涉及框架面板式卫星技术领域,提出一种框架面板式卫星的主框架,其特征在于,包括:框架,其包括多个杆件;以及连接部件,其连接所述框架。本发明采取模块化、标准化的设计理念,使用单一标准化的杆件以及连接部件,可以用于构造1吨以内的不同卫星平台的主框架或者用于更大重量的大型卫星的载荷舱,可以使得卫星的设计成本与制造成本大大降低,从而为卫星平台的批产化、标准化、低成本化打下基础。通过本发明的技术方案,可以使卫星的主框架成本至少降低八成,具有良好的经济效益。


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    Titel :

    Main frame of frame panel type satellite


    Weitere Titelangaben:

    一种框架面板式卫星的主框架


    Beteiligte:
    CHENG ZESONG (Autor:in) / SHEN YUAN (Autor:in) / JIANG GUIZHONG (Autor:in) / CHEN HONGCHENG (Autor:in) / TIAN YAN (Autor:in) / CAO DONGDONG (Autor:in) / LIU JIAWEI (Autor:in) / XIE FANG (Autor:in) / GUAN SHUJUN (Autor:in)

    Erscheinungsdatum :

    2023-06-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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