An aircraft includes a wing and a leading-edge aerodynamic surface coupled to the wing. An actuator is disposed within the wing and coupled to the leading-edge aerodynamic surface via a linkage system. Two or more hinge systems are coupled to the leading-edge aerodynamic surface and configured to rotate about a fixed axis internal to the wing to move the leading-edge aerodynamic surface between a retracted position and a drooped position.


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    Titel :

    LEADING-EDGE DROOP ACTUATION SYSTEM


    Weitere Titelangaben:

    VORDERKANTENBETÄTIGUNGSSYSTEM
    SYSTÈME D'ACTIONNEMENT DE BORD D'ATTAQUE


    Beteiligte:
    WYDOCK KYLE STEVEN (Autor:in) / BURIN RAMÓN (Autor:in) / STANDLEY JOHN A (Autor:in) / GOOD MARK STEVEN (Autor:in) / BLOCK SAMUEL (Autor:in)

    Erscheinungsdatum :

    11.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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