The invention discloses an aircraft modularization solution method and a modularized aircraft; the aircraft includes a drive device module 1, a connection module 2, a carrying module 3 and an auxiliary module 4; the drive device module 1 and the carrying module 3 are combined into an aircraft structural unit through the connection module 2; while carrying energy and load, the carrying module 3 also is used as an aircraft fuselage structure; the structural unit can be optionally added with the auxiliary module 4 used for filling up the deficiency of the modules. The modularized aircraft manufactured according to the method has the energy and load distribution redistributed, the structure power transmission path is changed, and the stress distribution between structures is optimized, so that the problems of complicated mechanical structure and concentrated load of a traditional aircraft are solved, and the aircraft structure can be infinitely benignly developed according to needs. In addition, with adopting of the modularization combined structure, components and parts in the aircraft are generalized and standardized.


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    Titel :

    Aircraft modularization solution method and modularized aircraft


    Beteiligte:
    TIAN YUEFENG (Autor:in)

    Erscheinungsdatum :

    09.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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