High-wind-resistance distributed propulsion aircraft

The invention belongs to the technical field of airplanes, and discloses a high-wind-resistance distributed propulsion aircraft. The aircraft comprises a fuselage, wings, an empennage and distributed propellers, the fuselage and the wings are fused in the middle of the fuselage, the fuselage is in a non-circular and non-flat U shape, the wings are divided into an inner wing, an outer wing and a small wing, the distributed propellers are symmetrically installed at the tail edge of the upper surface of the inner wing, and the empennage is arranged in a V-tail or pi-tail mode and installed above the tail of the fuselage. According to the high-wind-resistance distributed propulsion aircraft, through the fusion design of the aircraft body and the wings, the aircraft has small course static stability, through differential control of the distributed propellers, the aircraft has high course control capacity, and compared with an aircraft with a traditional layout, the aircraft has the advantages that the aircraft is