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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    Titel :

    AIRFOIL TRAILING EDGE HIGH-LIFT DEVICE AND ACTUATION SYSTEM THEREFORE


    Weitere Titelangaben:

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



    Erscheinungsdatum :

    2018-09-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



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