Example methods and apparatus for mitigating aerodynamic flutter of aircraft wing flaps are disclosed. An example apparatus includes a fairing, an actuator, and a damper. The fairing is located on a bottom side of a wing of an aircraft. The actuator is disposed in the fairing. The actuator is coupled to and extends between the wing and a flap of the wing. The damper is disposed in the fairing. The damper is coupled to and extends between the fixed wing and the moveable flap.


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    Titel :

    METHODS AND APPARATUS FOR MITIGATING AERODYNAMIC FLUTTER OF AIRCRAFT WING FLAPS


    Beteiligte:
    GOOD MARK S (Autor:in) / NGUYEN RENE T (Autor:in) / DEMPSTER GREGOR W (Autor:in) / GRUNER BRYAN J (Autor:in) / BAE KWAN-HO (Autor:in) / FAHEY PATRICK M (Autor:in)

    Erscheinungsdatum :

    2021-03-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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