An airplane wing assembly includes a wing, a winglet and a connection element. The wing has a wing box. The wing box is located at a wing tip of the wing and the winglet is connected with the wing by the wing box. The connection element includes a butt joint rib, which is assembled with the wing box, and a center connection, which is assembled with the winglet. The butt joint rib has a first shearing pin hole and a second shearing pin hole, into which are press fitted a corresponding first and a second shearing pin respectively to form interference fit. The center connector has a first sleeve hole and a second sleeve hole.


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    Titel :

    Aircraft wing assembly


    Beteiligte:
    LIAN WEI (Autor:in) / LI MING (Autor:in) / LIU JIANGANG (Autor:in) / WENG CHENTAO (Autor:in) / SHEN DEHONG (Autor:in) / LIU YANKAI (Autor:in) / HE RUI (Autor:in) / ZHANG YUANQING (Autor:in) / XU MENGMENG (Autor:in)

    Erscheinungsdatum :

    30.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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