The invention discloses a modular satellite structure device oriented to low cost, a plurality of module units, a body-mounted solar wing and an unfolded solar wing, every two module units are connected through a pin rod assembly, the body-mounted solar wing is fixedly mounted on the front surface of a module satellite composed of the plurality of module units, and the unfolded solar wing is fixedly mounted on the front surface of the module satellite. The unfolded solar wing is fixedly installed on the side wall of a module satellite composed of a plurality of module units through a center plate assembly. Through combination of the pin rod assemblies and the module units, combination between the module units is tighter and more stable, and combination accuracy can be guaranteed; through modular assembly, the modular units can be quickly assembled, and meanwhile, the overall research and development and production and manufacturing cost can be reduced through modular unit design; the identification blocks are arranged, so that automation can be realized in the splicing process; through the modular unit design, the modules can be quickly replaced, and the modules can be quickly maintained in a limited space, and are convenient and quick.

    本发明公开了面向低成本的模块化卫星结构装置,模块单元、体装太阳翼与展开太阳翼,所述模块单元为若干个,且每两个模块单元间通过销杆组件连接,所述体装太阳翼固定安装于若干模块单元组成的模块卫星前表面,所述展开太阳翼通过幅板组件固定安装于若干模块单元组成的模块卫星侧壁;通过销杆组件与模块单元的组合,使得模块单元间的组合更加紧密、稳定,且能保证组合精准;通过模块化拼装,使得模块单元间能够进行快速的拼装,同时模块单元化设计,能够降低整体的研发及生产制造成本;设置标识块,使得拼装过程中可以实现自动化;通过模块单元化设计,能够使得彼此间能够进行快速的更换,且在有限空间内能够进行快速的维修,方便快捷。


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    Titel :

    Modularized satellite structure device oriented to low cost


    Weitere Titelangaben:

    面向低成本的模块化卫星结构装置


    Beteiligte:
    CHANG ZHENGYONG (Autor:in) / ZHANG YABIN (Autor:in) / YANG JIAWEN (Autor:in)

    Erscheinungsdatum :

    2023-03-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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