The present invention relates to a panel, especially for a component having a box structure in an airplane airfoil, comprising a surface shaped body and grid-like reinforcement bars protruding from the body on one side of the body, and the body and the grid-like reinforcement bars are integral molded. Since the body and the grid-like reinforcement bars of the panel are integral molded, no additional connecting process is required, so that the disconnection phenomenon as happened between the skin and the stiffener or stringer of the prior art would not occur, and the assembly complexity can be decreased.


    Access

    Download


    Export, share and cite



    Title :

    Component having a box structure for an airplane airfoil


    Contributors:
    LI JUN (author)

    Publication date :

    2016-09-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Solar-powered airplane airfoil profile design method and solar-powered airplane airfoil profile

    ZENG HONGJIANG / BAI LIN / XIE JINDONG | European Patent Office | 2015

    Free access

    Airplane airfoil panel structure and forming method thereof

    JIN AN / WANG XINNIAN / CHEN LI et al. | European Patent Office | 2024

    Free access

    Airplane airfoil part load calculation method

    YANG QUAN / GUO SHAONAN / LIU WEI et al. | European Patent Office | 2024

    Free access

    Airplane airfoil type composite material wingtip structure and manufacturing method

    JIANG SHAN / CUI XIAOZHAN / QI XIAOPENG | European Patent Office | 2022

    Free access

    Airfoil component having electrochemically insulating layer

    WATSON THOMAS J | European Patent Office | 2022

    Free access