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.
TILTROTOR AIRCRAFT
KIPPROTORFLUGZEUG
AÉRONEF À ROTORS BASCULANTS
2024-10-23
Patent
Electronic Resource
English