The invention provides a fuselage skeleton structure. The fuselage skeleton structure comprises a plurality of annular supporting parts (210) and a connecting part (220), wherein the multiple annularsupporting parts (210) are sequentially arranged in the length direction of a fuselage and used for forming the outline of the fuselage, and the connecting part (220) sequentially penetrates through the multiple annular supporting parts (210) and is connected with the multiple annular supporting parts (210). On the other hand, the invention provides the fuselage and an aircraft.

    本公开提供了一种机身骨架结构,包括:多个环形支撑部件(210),所述多个环形支撑部件(210)沿机身的长度方向依次排列,用于形成所述机身的轮廓;以及连接部件(220),所述连接部件(220)依次穿过所述多个环形支撑部件(210),并与所述多个环形支撑部件(210)连接。本公开的另一方面还提供了一种机身和一种飞行器。


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    Title :

    Fuselage skeleton structure, fuselage and aircraft


    Additional title:

    机身骨架结构、机身和飞行器


    Contributors:
    XU JINHAO (author) / ZHANG XIANG (author) / LI JIANING (author)

    Publication date :

    2020-12-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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