| 摘要 |
<p>A propeller vertical takeoff and landing aircraft with a fairing device, comprises a fuselage (1), a control device, a power device and a propeller (2), wherein the control device and the power device are arranged in the fuselage, and the propeller is arranged above the fuselage. It is characterized in that the aircraft also comprises a fairing device (3) which comprises at least two fairing plates (31, 32) in shape of a flat plate band, the plane of the flat plate is parallel to the axial direction of the aircraft screw axis, namely, vertical to a rotary plane of the propeller, and the fairing plates are intercrossedly arranged below the fuselage. It is an object of the invention to provide a propeller vertical takeoff and landing aircraft which does not generate left and right torsion pendulum during takeoff and landing, flying and hovering, and can steadily take off and land vertically, fly and hover. It can ensure stable condition of the aircraft to a certain degree in emergency, and has functions of safety and energy conservation.</p> |
