A composite flexure that secures a rotor blade to a gimbaled yoke in a tiltrotor rotor system. The composite flexure includes a composite flexure member, a first end, and a second end. The first end of the composite flexure couples the composite flexure to the gimbaled yoke, and the second end of the composite flexure couples the composite flexure to the rotor blade. The composite flexure is twisted when the composite flexure is not subject to torsional loads in order to accommodate various forces imparted on the rotor system.


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    Titel :

    Composite flexure for tiltrotor rotor system


    Beteiligte:
    FOSKEY CHRISTOPHER (Autor:in) / STAMPS FRANK B (Autor:in) / MCINTYRE JOEL (Autor:in) / MILLER GARY (Autor:in)

    Erscheinungsdatum :

    22.11.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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