Wing-engine corotating vertical takeoff and landing aircraft with partially fixed wings

Abstract

A wing-engine corotating vertical takeoff and landing aircraft with partially fixed wings is provided. The aircraft includes an aircraft fuselage, and front wings and rear wings arranged on the aircraft fuselage. Each of the front wings and the rear wings includes a fixed wing connected with the aircraft fuselage, and a tiltwing is hinged with an end, away from the aircraft fuselage, of the fixed wing. A rotational axis of the tiltwing extends horizontally inward and is perpendicular to an axis of the aircraft fuselage. Each tiltwing is provided with a propeller tilting along with the tiltwing. Geometrically, one end of a rotating shaft of the propeller is arranged on the tiltwing, and the other end of the rotating shaft of the propeller extends along the advancing or ascending direction of the aircraft fuselage, and the rotating shaft forms a negative angle with the plane where the tiltwing is located.

Dependencies are inferred from the claim text.