A tiltrotor aircraft includes a fuselage; a wing member having a first rib, a second rib, a first spar, second spar; and an upper wing skin; an engine disposed at a fixed location relative to the wing member; and a proprotor having a spindle gearbox, rotor mast, and a plurality of rotor blades drivable in rotation about the rotor mast, the spindle gearbox being rotatable about a conversion axis. The spindle gearbox is located above the upper wing skin of the wing member.


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    Titel :

    Fixed engine and rotating proprotor arrangement for a tiltrotor aircraft


    Beteiligte:
    ROSS BRENT C (Autor:in) / BOCKMILLER DAVID R (Autor:in) / MCCULLOUGH JOHN R (Autor:in) / CARLSON DAVID G (Autor:in)

    Erscheinungsdatum :

    2015-11-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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