The invention discloses a high-adaptability point location array type child-mother satellite mounting interface system which comprises an adapter panel arranged on a child satellite or a mother satellite, a plurality of mounting holes are prefabricated in the adapter panel, and the mounting holes are all used for mounting a separation mechanism and are distributed in a plurality of concentric circles with the geometric center of the adapter panel as the circle center. A plurality of mounting holes are formed in the same concentric circle at equal intervals, the positions of the mounting holes, where the separation mechanisms need to be mounted, in the transfer panel are determined firstly according to the positions of the interfaces in the mother satellite or the child satellite to be butted, the separation mechanisms are mounted in the corresponding positions, and then the child satellite and the mother satellite are butted by means of the assembled transfer panel; or according to the position of the interface on the mother satellite or the child satellite to be butted, the position where the separation mechanism needs to be installed on the switching panel is determined firstly, then holes are directly formed in the corresponding position of the switching panel, then the separation mechanism is installed, and finally the child satellite and the mother satellite are butted by means of the assembled switching panel.

    本发明公开了一种高适应性点位阵列式子母星挂载接口系统,包括设置在子星或母星上的转接面板,在所述转接面板上预制有多个安装孔,这些安装孔均用于安装分离机构,且分布在以转接面板的几何中心为圆心的多个同心圆上,同一个同心圆上的多个安装孔均匀间隔排列,根据待对接的母星或者子星上的接口位置,先确定转接面板上需要安装分离机构的安装孔位置,并在对应位置上安装好分离机构,再借助装配好的转接面板,实现子母星对接;或者根据待对接的母星或者子星上的接口位置,先确定转接面板上需要安装分离机构的位置,然后在转接面板的对应位置上直接开孔,再安装好分离机构,最后借助装配好的转接面板,实现子母星对接。


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    Titel :

    High-adaptability point location array type child-mother satellite mounting interface structure


    Weitere Titelangaben:

    一种高适应性点位阵列式子母星挂载接口结构


    Beteiligte:
    CHENG PENGHUI (Autor:in) / ZHANG KEKE (Autor:in) / ZHOU MEIJIANG (Autor:in) / ZHANG TIANHE (Autor:in) / ZHU YONGSHENG (Autor:in)

    Erscheinungsdatum :

    27.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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