Airfoil trailing edge high-lift device comprising at least one flap, wherein said flap is movable between a retracted position and at least one deployed position, and is arranged to be actuated by an actuation system comprising at least one rib which is mountable to an airfoil, wherein the rib comprises a track along which the trailing edge high-lift device is adjustable between a retracted position in which the trailing edge high-lift device is substantially partly inside the airfoil, and at least one deployed position in which the trailing edge high-lift device is substantially outside of the airfoil; comprising an adjustment mechanism arranged to adjust the trailing edge high-lift device along the track.


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    Title :

    AIRFOIL TRAILING EDGE HIGH-LIFT DEVICE AND ACTUATION SYSTEM THEREFORE


    Additional title:

    TRAGFLÄCHENHINTERKANTENAUFTRIEBERHÖHUNGSVORRICHTUNG UND BETÄTIGUNGSSYSTEM DAFÜR
    DISPOSITIF HYPERSUSTENTATEUR DE BORD DE FUITE À PROFIL AÉRODYNAMIQUE ET SYSTÈME D'ACTIONNEMENT CORRESPONDANT



    Publication date :

    2018-09-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



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