Novel tilt wing aircraft

The invention discloses a novel tilt wing aircraft, which is capable of carrying out vertical take-off, landing and hovering, capable of flying in a fixed wing airscrew aircraft mode, and also capable of switching between two modes. The aircraft mainly consists of an aircraft structure, a connection structure and a flying control system, wherein aircraft wings are divided into a fixed part and a movable part; when the aircraft takes off, lands and hovers, the movable wings and non-variable torque airscrew systems fixed to the movable wings tilt along a rotating shaft to a vertical state, and a lift force is provided by airscrews; when the aircraft is in flat flight, the movable wings and the airscrew systems rotate to the fixed wing part, and the aircraft flies like a normal layout fixed wing aircraft; in a switching phase, the aircraft is controlled by the flying control system which is independently researched. The aircraft has the characteristics that the functions are many, the use range is wide, the structure is simple, the cost is low and the like, and can be widely applicable to fields of air photography, expressway patrol, disaster situation reconnaissance, military reconnaissance and the like.