Example methods and apparatus for mitigating aerodynamic flutter of aircraft (100) wing (104, 106) flaps (112) are disclosed. An example apparatus includes a fairing (200), an actuator (400), and a damper (600, 1300, 1400). The fairing (200) is located on a bottom side (210, 212) of a wing (104, 106) of an aircraft (100). The actuator (400) is disposed in the fairing (200). The actuator (400) is coupled to and extends between the wing (104, 106) and a flap (112, 114) of the wing (104, 106). The damper (600, 1300, 1400) is disposed in the fairing (200). The damper (600, 1300, 1400) is coupled to and extends between the fixed wing (104, 106) and the moveable flap (112, 114).


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    Titel :

    METHODS AND APPARATUS FOR MITIGATING AERODYNAMIC FLUTTER OF AIRCRAFT WING FLAPS


    Weitere Titelangaben:

    VERFAHREN UND VORRICHTUNG ZUR ABSCHWÄCHUNG VON AERODYNAMISCHEM FLATTERN VON FLUGZEUGFLÜGELKLAPPEN
    PROCÉDÉS ET APPAREIL POUR ATTÉNUER LE FLOTTEMENT AÉRODYNAMIQUE DE VOLETS D'AILE D'AÉRONEF


    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 :

    03.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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