VERTICAL TAKEOFF AND LANDING AIRCRAFT THAT CAPABLE OF TRANSITION FLIGHT

摘要

PURPOSE: A vertical takeoff and landing aircraft capable of transition flight is provided to stably fly without low energy in transition flight by integrating multiple blades on the exterior of a duct in a single body. CONSTITUTION: A vertical takeoff and landing aircraft capable of transition flight comprises an annular duct, a rotor assembly, a stator assembly(3), a control vane assembly(4), and a battery mount(5). The rotor assembly comprises a propeller rotated forward and backward by the power of a motor and is installed in the internal space of the duct. The stator assembly damps the reaction movement of the duct when the propeller rotates. The control assembly variously converts thrust deducted directions generated by the rotation of the propeller. The battery mount is supported and fixed by the rotor assembly and a battery(6) for driving the motor is loaded thereon.