Embodiments include an aircraft comprising a fuselage; a wing connected to the fuselage; and first and second propulsion systems connected to the wing on opposite sides of the fuselage, wherein at least a portion of each of the first and second propulsion systems and at least a portion of the wing are tiltable between a first position in which the aircraft is in a hover mode and a second position in which the aircraft is in a cruise mode, wherein each of the propulsion systems includes pylon and a rotor assembly comprising a plurality of rotor blades.


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    Titel :

    ELECTRIC TILTROTOR AIRCRAFT


    Beteiligte:
    ROSS BRENT C (Autor:in) / GRONINGA KIRK L (Autor:in) / IVANS STEVEN R (Autor:in) / HURST JASON PAUL (Autor:in)

    Erscheinungsdatum :

    2023-11-02


    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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