Overview
The present invention relates to a novel adjustable aircraft propeller/rotor assembly for multi-dimensional movement which is capable of vertical takeoff and landing, includes a fuselage without control surfaces. The tilt rotor assembly is mounted within the duct which is formed through each wing for providing downward thrust causing lift. Each propeller is mounted on the circular ring and engages with the rotor assembly. The present invention uses the same tilt rotor assembly to provide vertical takeoff, forward thrust along the longitudinal axis of the aircraft as well as yaw. The tilt rotor assembly includes a drive shaft and its engine.