A flexible joint assembly for providing flexure to a rotor blade comprising an upper hub plate and a lower hub plate configured to secure a rotor blade yoke via a bolted joint located radially outward of a mast; and an upper flexure assembly connected to the upper hub plate and a lower flexure assembly connected to the lower hub plate, wherein the upper flexure assembly and lower flexure assembly are configured to promote flapping of the rotor blade yoke about a flapping hinge located radially outward of the bolted joint.


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    Titel :

    Flexing clevis arrangement bolted joint attachment for flexible rotor hub with high offset and high flapping


    Beteiligte:
    SUTTON DREW (Autor:in) / STAMPS FRANK B (Autor:in) / TISDALE PATRICK RYAN (Autor:in) / OLDROYD PAUL (Autor:in)

    Erscheinungsdatum :

    2016-11-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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