A tiltrotor aircraft includes a fuselage, a wing member extending from the fuselage, an engine disposed relative to the wing member and a proprotor mechanically coupled to the engine. The proprotor includes a plurality of proprotor blade assemblies each including a spar and a sheath extending spanwise along the spar forming the leading edge of the proprotor blade assembly. The spar has a root section, a main section and a tip section. The spar has a generally oval cross section at radial stations along the main section and a first edge having a structural bias relative to a generally oppositely disposed second edge at the radial stations along the main section.


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    Titel :

    Structurally Biased Proprotor Blade Assembly


    Beteiligte:
    FOSKEY CHRISTOPHER (Autor:in) / BURNETT MICHAEL (Autor:in) / BOSWORTH JEFFREY (Autor:in) / PAULSON JARED MARK (Autor:in) / MCINTYRE JOEL (Autor:in) / OLDROYD PAUL K (Autor:in)

    Erscheinungsdatum :

    2017-11-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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