A rotor system for tilt rotor aircraft comprises an engine disposed at a first fixed location on a wing member; a prop-rotor pylon mechanically coupled to the engine along a drive path, and a gearbox disposed in the drive path. The prop-rotor pylon is rotatably mounted on a spindle, and the prop-rotor pylon is configured to selectively rotate about a rotational axis of the spindle between a vertical position and a horizontal position. The gearbox comprises a rotational axis aligned with the rotational axis of the spindle.


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    Titel :

    Spindle mounted tiltrotor pylon with fixed engine arrangement


    Beteiligte:
    ROSS BRENT C (Autor:in) / BOCKMILLER DAVID R (Autor:in) / ISAAC MARK L (Autor:in) / COX BRIAN J (Autor:in)

    Erscheinungsdatum :

    2015-09-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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