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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    Titel :

    LEADING EDGE ASSEMBLY FOR AN AIRCRAFT


    Weitere Titelangaben:

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


    Beteiligte:

    Erscheinungsdatum :

    2017-02-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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