The invention provides a satellite installation and adjustment method for a large-size plate type main load-bearing structure. According to the method, the mode that the force bearing plates are spliced one by one is adopted, and in the splicing process, the assembling direction of the force bearing plates to be assembled is controlled, so that the problem that the mounting surface of the instrument equipment is deformed due to the fact that the force bearing plates are influenced by ground gravity in the assembling process is solved. And the structural stability of the force bearing structure is ensured. The method has the advantages of being high in practicability, easy and convenient to operate and high in efficiency, and meets the requirement of a satellite for the stability of a load-bearing structure.

    本发明提出一种大尺寸板式主承力结构的卫星装调方法。所述方法采用了承力板逐一拼接的方式,通过拼接过程中,控制待装配承力板装配方向,减少承力板在装配过程中受地面重力影响而导致的仪器设备安装面变形的问题。保证了承力结构的结构稳定性。具有可实施性强,操作简便、效率高的特点,满足了卫星对承力结构稳定性的要求。


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    Titel :

    Satellite installation and adjustment method for large-size plate-type main load-bearing structure


    Weitere Titelangaben:

    一种大尺寸板式主承力结构的卫星装调方法


    Beteiligte:
    GAO FEI (Autor:in) / ZHANG LEI (Autor:in) / CHEN SHANBO (Autor:in) / ZHANG CHENGZE (Autor:in) / LIU CONG (Autor:in)

    Erscheinungsdatum :

    15.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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