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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    Titel :

    Novel connection structure for aircraft body and aircraft wings


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

    Erscheinungsdatum :

    09.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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