Embodiments include an aircraft (400) comprising: a fuselage (402); a wing (404a, 404b) connected to the fuselage (402); and first and second propulsion systems (408a, 408b, 412a, 412b) connected to the wing on opposite sides of the fuselage (402), wherein at least a portion of each of the first and second propulsion systems (408a, 408b, 412a, 412b) are tiltable between a first position in which the aircraft (400) is in a hover mode and a second position in which the aircraft is in a cruise mode; wherein each of the first and second propulsion systems (408a, 408b, 412a, 412b) includes pylon and a rotor assembly comprising a plurality of rotor blades.


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    Title :

    TILTROTOR AIRCRAFT


    Additional title:

    KIPPROTORFLUGZEUG
    AÉRONEF À ROTORS BASCULANTS


    Contributors:
    ROSS BRENT (author) / GRONINGA KIRK (author) / IVANS STEVEN (author) / HURST JASON (author)

    Publication date :

    2024-10-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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