The invention provides a novel connection structure for an aircraft body and aircraft wings. Connector structures are additionally arranged on a conventional structure of a central wing front beam and a central wing rear beam of the aircraft body, besides the matched connector structures are arranged at positions corresponding to the central wing front beam and the central wing rear beam of the aircraft body of the aircraft wings, and aircraft body connectors and aircraft wing connectors are connected and fixed through bolts, so that the aircraft wings are disassembled.


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    Title :

    Novel connection structure for aircraft body and aircraft wings


    Contributors:
    WU GENLIN (author) / DENG CHENGYANG (author) / JI XIANWU (author) / XU HUANYU (author) / HU DINGHONG (author) / XIONG YI (author) / ZHANG WEI (author) / WANG BIN (author)

    Publication date :

    2015-09-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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