The invention discloses a satellite standard structure and a frame structure, and relates to the technical field of satellite structure design. One specific embodiment of the satellite standard structure comprises a main frame and at least one group of ejection assemblies, the ejection assembly is installed on the bottom face or the side face or the top face of the main frame and comprises an ejector adapter, an unlocking base, an explosive bolt or a separation nut and an ejection base. The ejection base is installed on the bottom face or the side face or the top face of the main frame and used for installing the ejection base on the main frame, the unlocking base is assembled on the ejection base; the explosive bolt or the separating nut is arranged on the unlocking base and used for being connected with main frames of other satellite frame structures. By adopting the satellite standard structure provided by the invention, a required structural space can be conveniently spliced, and the trouble of designing a personalized structure for each satellite is avoided; according to the frame structure, satellites are connected and reinforced with one another, so that the weight consumedfor independently supporting the satellite structure is saved.

    本发明公开了一种卫星标准结构和框架结构,涉及卫星结构设计技术领域。该卫星标准结构的一具体实施方式包括:主框架和至少一组弹射组件;其中,弹射组件安装于主框架的底面或侧面或顶面上,包括:弹射器转接座、解锁座、爆炸螺栓或分离螺母、弹射座;弹射器转接座安装于主框架的底面或侧面或顶面上,用于将弹射座安装在主框架上;解锁座装配于弹射座上;爆炸螺栓或分离螺母设置在解锁座上,用于与其他卫星框架结构的主框架连接。采用本发明的卫星标准结构能够方便的拼接出所需要的结构空间,免去了为每颗卫星设计个性结构的麻烦;本发明的框架结构采用卫星之间互相连接、互相加强的方式,省去了独立支撑卫星结构所耗费的重量。


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    Titel :

    Satellite standard structure and frame structure


    Weitere Titelangaben:

    一种卫星标准结构和框架结构


    Beteiligte:
    CHEN JINLIN (Autor:in)

    Erscheinungsdatum :

    2021-01-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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