A leading edge high-lift device (22), that may be deployable from a wing (12) of an aircraft, may include a leading edge (26) and a trailing edge (28). A lower surface (32) and an upper surface (30) may both extend between the leading edge (26) and the trailing edge (28). A trailing edge region (34) may be defined by the trailing edge (28) and an adjacent region thereto. A shaping device (36) may be disposed at the trailing edge region (34) and may be movable between a non-activated position and an activated position.


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    Title :

    LEADING EDGE HIGH-LIFT DEVICE


    Additional title:

    VORDERKANTENAUFTRIEBSERHÖHENDE VORRICHTUNG
    DISPOSITIF HYPERSUSTENTATEUR DE BORD D'ATTAQUE



    Publication date :

    2019-11-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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