A rotor system for tilt rotor aircraft comprises an engine disposed at a first fixed position on a wing member, and a prop-rotor pylon mechanically coupled to the engine along a drive path extending through the wing member. The engine is disposed adjacent a fuselage of the tilt rotor aircraft, and the prop-rotor pylon is configured to selectively rotate between a vertical position and a horizontal position. The prop-rotor pylon is coupled to a plurality of rotor blades.


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    Titel :

    Tiltrotor aircraft with inboard wing mounted 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 :

    28.06.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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