Systems and methods provide for the mitigation of vibrational forces acting on a horizontal stabilizer of an aircraft. According to one aspect, a damper is coupled to a front portion of a horizontal stabilizer to dampen vibrations in a first degree of freedom, with another damper coupled to a mounting point of the horizontal stabilizer to dampen vibrations in a second degree of freedom. The dampers may be passive, operating independently to mitigate vibrational forces, or active, applying a mitigating force to the horizontal stabilizer based on real-time or estimated vibration states.


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    Titel :

    VIbration Dampening For Horizontal Stabilizers


    Beteiligte:
    GOLSHANY SINA SAM (Autor:in) / ERICKSON TODD W (Autor:in) / TRETOW PAUL R (Autor:in) / HUNTLY DAVID M (Autor:in)

    Erscheinungsdatum :

    2016-11-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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