A wing assembly includes a main wing (500) and a slat (510) movable between stowed and deployed positions. The main wing (500) includes a panel (512) movable to a retracted position when the slat (510) is in the stowed position, such that the slat outer surface (514) and a wing upper surface (503) define a first continuous outer mold line shape. The panel (512) may further be movable to an extended position when the slat (510) is in the deployed position, such that an outer surface (525) of the panel (512) and the wing upper surface (503) define a second continuous outer mold line shape.


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    Title :

    LEADING EDGE ASSEMBLY FOR AN AIRCRAFT


    Additional title:

    VORDERKANTENANORDNUNG FÜR EIN FLUGZEUG
    ENSEMBLE DE BORD D'ATTAQUE POUR UN AVION


    Contributors:

    Publication date :

    2017-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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