ELECTRIC TILTROTOR AIRCRAFT

Abstract: 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.

Inventor(s): Brent C. Ross, Kirk L. Groninga, Steven R. Ivans, Jason Paul Hurst

CPC Classification: B64C29/0033 (Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft (rotorcraft ))

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