The invention relates to the technical field of aircrafts, in particular to a tilt rotor aircraft. The tilt-rotor aircraft comprises a fuselage, canards, main wings, a first tilt-rotor group, a second tilt-rotor group and a third tilt-rotor group, the canards are arranged at the nose of the fuselage, the main wings are arranged at the tail of the fuselage, the first tilt-rotor group is arranged on the canards, the second tilt-rotor group and the third tilt-rotor group are arranged on the main wings, and the second tilt-rotor group and the third tilt-rotor group are arranged at the tail of the fuselage. The first tilting wing set is located on the axis of the mass center of the aircraft, the second tilting wing set is located on the axis of the mass center of the aircraft, and projections of at least four tilting wings in the first tilting wing set, the second tilting wing set and the third tilting wing set on the horizontal plane form a parallelogram with the mass center of the aircraft as the center. According to the aircraft, the canard wings are matched with the four balance tilting wings, so that the flight performance and the flight safety of the aircraft can be improved.
本发明涉及飞行器技术领域,尤其涉及一种倾转旋翼飞行器。所述倾转旋翼飞行器,包括机身、鸭翼、主翼、第一倾转翼组、第二倾转翼组及第三倾转翼组,所述鸭翼设于所述机身的机头,所述主翼设于所述机身的机尾,所述第一倾转翼组设于所述鸭翼,所述第二倾转翼组和所述第三倾转翼设于所述主翼,且且所述第二倾转翼组位于所述飞行器的质量中心的轴线上,其中,所述第一倾转翼组、所述第二倾转翼组及所述第三倾转翼组中的至少四个倾转翼于水平面的投影构成以所述飞行器的质量中心为中心的平行四边形。本发明的飞行器通过鸭翼配合四平衡倾转翼,可以提高所述飞行器的飞行性能及飞行安全性。
Tilt-rotor aircraft and control method thereof
倾转旋翼飞行器及其控制方法
2024-12-13
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |