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.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft modularization solution method and modularized aircraft


    Contributors:

    Publication date :

    2015-12-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Modularized wing angle aircraft

    XU XING / BING FUQIANG | European Patent Office | 2023

    Free access

    Modularized aircraft assembly working platform

    YE LIN / HUANG RUXUE / WANG ZHENWEN et al. | European Patent Office | 2021

    Free access

    EICAS as a Modularized Aircraft System

    Kennell, Steven M. | SAE Technical Papers | 1991


    Modularized reconfigurable wide-working-condition aircraft

    FAN LI / WEN GUANGWEI | European Patent Office | 2025

    Free access

    Plug type modularized multi-rotor aircraft frame

    YU ZHAOBING / GAO LU / YAN HUA et al. | European Patent Office | 2015

    Free access