A blade retention system includes a rotor hub including a plurality of radial arms, and a blade retention yoke associated with the rotor hub and one of the plurality of radial arms. The blade retention yoke is rotatable relative to the rotor hub and the radial arm. A tension torsion device connects the radial arm to the blade retention yoke to restrict radial movement of the blade retention yoke relative to the radial arm.


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    Titel :

    BLADE RETENTION SYSTEM FOR RIGID ROTOR


    Beteiligte:
    MINER FREDERICK J (Autor:in) / BOWMAN RODGER W (Autor:in) / POULIN STEPHEN V (Autor:in) / BYRNE ERIK M (Autor:in) / COWLES DEVON K (Autor:in) / HOOD RICHARD THOMAS (Autor:in)

    Erscheinungsdatum :

    2019-09-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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