The invention discloses a satellite module rapid butt joint and separation structure and a using method, the satellite module rapid butt joint and separation structure comprises a parent body and a child body, the parent body is provided with a first adapter block, a magnet array, a heating sheet and a positioning bolt, one end, close to the child body, of the first adapter block is provided with a first cone-frustum-shaped groove, and the narrower end of the first groove is provided with a second cuboid-shaped groove. And the heating sheet and the magnet array are embedded in the groove II. The rapid butt joint and separation structure is low in production cost, simple in structure, short in period and capable of being produced in batches; reliability is high, bearing capacity is high, and energy consumption is low; through butt joint and separation between the parent body and the child body, the structure is high in butt joint and separation speed, high in assembly efficiency and capable of being repeatedly and rapidly disassembled for multiple times; the requirements of various products and facility instruments in space, on the sea and on the land on docking, separating, assembling, transporting, testing and the like can be met, and the application range is wide; and a magnetic array structure non-moment design is adopted, so that magnetic influence on surrounding components is avoided.

    本发明公开了一种卫星模块快速对接与分离结构及使用方法,包括母体和子体,所述母体设有转接块一、磁体阵列、加热片和定位栓,所述转接块一靠近子体一端开设有圆锥台形状的凹槽一,所述凹槽一较窄一端开设有长方体形状的凹槽二,所述加热片和磁体阵列嵌设于凹槽二内。本发明中,快速对接与分离结构生产成本低、结构简单、周期短、可批量化生产;可靠性高,承载力强,能量消耗低;通过母体与子体之间的对接与分离,使得本结构对接和分离速度快,装配效率高,可多次重复快速拆卸;可满足空间、海上和陆地各种产品、设施仪器对接分离,组装、运输、测试等过程需要,用途广;采用磁阵列结构无矩设计,不会对周围部件产生磁影响。


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    Titel :

    Satellite module rapid butt joint and separation structure and use method


    Weitere Titelangaben:

    一种卫星模块快速对接与分离结构及使用方法


    Beteiligte:
    XU CHAOQUN (Autor:in) / HUANG KUI (Autor:in) / YI ZHONG (Autor:in) / DENG WEIHUA (Autor:in) / XIAO QI (Autor:in) / WANG BIN (Autor:in) / GAO YANG (Autor:in) / LIU CHAOBO (Autor:in) / GENG XIAOLEI (Autor:in) / ZHANG YANJING (Autor:in)

    Erscheinungsdatum :

    2023-08-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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