A tiltrotor aircraft includes a fuselage supporting first and second wings each having an outboard end. First and second nacelles are respectively coupled to the outboard ends of the first and second wings. The first and second nacelles each have an outboard end. First and second wing extensions are rotatably coupled, respectively, to the outboard ends of the first and second nacelles. First and second actuators are operable to respectively move the first and second wing extensions to dampen a mode of the first and second wings, thereby stabilizing the tiltrotor aircraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Tiltrotor aircraft having active wing extensions


    Beteiligte:

    Erscheinungsdatum :

    07.05.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Tiltrotor Aircraft having Active Wing Extensions

    BOSWORTH JEFFREY | Europäisches Patentamt | 2018

    Freier Zugriff

    Tiltrotor Aircraft having Rotatable Wing Extensions

    IVANS STEVEN RAY / WU NATHAN GABRIEL | Europäisches Patentamt | 2018

    Freier Zugriff

    Tiltrotor aircraft having rotatable wing extensions

    IVANS STEVEN RAY / WU NATHAN GABRIEL | Europäisches Patentamt | 2018

    Freier Zugriff

    Tiltrotor aircraft having rotatable wing extensions

    IVANS STEVEN RAY / WU NATHAN GABRIEL | Europäisches Patentamt | 2019

    Freier Zugriff

    Tiltrotor Aircraft having Rotatable Wing Extensions

    IVANS STEVEN RAY / WU NATHAN GABRIEL | Europäisches Patentamt | 2018

    Freier Zugriff