A rotor blade assembly includes a blade body having a leading edge and a trailing edge. A damper element is disposed within the blade body and along a forcing axis extending between the leading and trailing edges of the blade body to apply damping force in-plane with the blade body to damp load and oppose edgewise motion of the blade body associated with the load.


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    Titel :

    SYSTEMS AND METHODS FOR DAMPING ROTOR BLADE ASSEMBLIES


    Beteiligte:

    Erscheinungsdatum :

    09.02.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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