Vertical take-off and landing aircraft

The utility model relates to the technical field of flight, in particular to a vertical take-off and landing aircraft which comprises an aircraft body, a front wing and a rear wing which are arranged on the aircraft body, and a lifting frame connected with the front wing, a plurality of lifting propellers are arranged on the lifting frame; a plurality of thrust propellers are arranged on the rear wings and distributed on the two sides of the fuselage. A plurality of thrust propellers are arranged on the rear wings and are arranged on the two sides of the fuselage, and the thrust propellers provide power for flight of the aircraft, so that the aircraft is strong in power; when the aircraft flies in an arc-shaped track, the pushing power of the thrust propeller on any side can be selected and adjusted, and stable flight is facilitated; the lifting frame is arranged on the front wing, and the lifting propellers are arranged on the lifting frame, so that the aircraft realizes stable vertical take-off and landing,