Thrust type tilt rotor aircraft

A thrust type tilt rotor aircraft comprises a fuselage, rotors, wings, empennages, a tail rotor system, a landing gear and a power system. A left rotor and a right rotor are bilaterally symmetrically installed on the wings on the both sides of the fuselage through a left rotor tilt mechanism and a right rotor tilt mechanism by taking the fuselage axis as the center line, a tail rotor is installed at the tail of the fuselage through a tail rotor tilt mechanism, each of the left rotor tilt mechanism, the right rotor tilt mechanism and the tail rotor tilt mechanism comprises a tilt base, a steering engine and a link mechanism connected between the tilt base and the steering engine, the left rotor, the right rotor and the tail rotor are fixedly on the tilt bases of the left rotor tilt mechanism, the right rotor tilt mechanism and the tail rotor tilt mechanism, and the steering engines can drive the link mechanisms to further pull the tilt bases to realize the tilting of the rotors on the tilt bases. The aircraft stably realizes the transformation between multi-rotors and fixed wings, so that the resistance during forwards flight is reduced, and the propulsion efficiency is improved.