An aircraft including a flap support assembly for a flap support. An aircraft includes a fuselage comprising a pressure deck, where at least a portion the pressure deck is substantially horizontal. The aircraft further includes a wing extending from the fuselage, where the wing includes a leading edge and a trailing edge. The wing additionally includes a flap assembly on the trailing edge of the wing, where the flap assembly is configured to move between an extended position and a retracted position. The aircraft further includes a flap support coupled to the flap assembly comprising a plurality of load-bearing connection points, where at least one of the load-bearing connection points is coupled to the pressure deck.


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    Title :

    AIRCRAFT WING FLAP SUPPORT


    Additional title:

    FLUGZEUGFLÜGELKLAPPENSTÜTZE
    SUPPORT DE VOLET D'AILE D'AÉRONEF


    Contributors:
    TSAI KEVIN (author) / JOHNSON KYLE (author)

    Publication date :

    2022-03-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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