The invention relates to a tilt rotor unmanned aerial vehicle, and relates to the field of airplanes, the tilt rotor unmanned aerial vehicle comprises a fuselage and two combined wings, the two combined wings are symmetrically arranged about the fuselage axis, and each combined wing comprises a wing and a rotor; the unmanned aerial vehicle further comprises a driving assembly, the driving assembly is installed on the vehicle body and connected with the two wings correspondingly, and under driving of the driving assembly, the two wings synchronously rotate in the space along the vehicle body, so that the wings are transitionally converted between the first posture and the second posture; the first posture is a state that the wings are horizontal and are vertical to the axis of the fuselage when the airplane flies straightly; the second posture is that the wings are vertical and parallel to the axis of the fuselage when the aircraft takes off and lands vertically. The method has the effect that the lifting posture of the aircraft is more flexible and smoother.
本申请涉及一种倾转旋翼无人机,涉及飞机的领域,其包括机身、两个组合翼,两个组合翼关于所述机身轴对称设置,所述组合翼包括机翼和旋翼;还包括驱动组件,所述驱动组件安装于所述机身上,并与两个所述机翼分别连接,在所述驱动组件的驱动下,两个机翼在空间内沿所述机身同步旋转,从而使机翼在第一姿态和第二姿态之间过渡变换;所述第一姿态为飞机直飞时,所述机翼水平且与所述机身的轴线垂直的状态;所述第二姿态为飞机垂直起降时,所述机翼竖直且与所述机身的轴线平行的状态。本申请具有使得飞机的升降姿态更加灵活顺畅的效果。
Tilt rotor unmanned aerial vehicle
一种倾转旋翼无人机
2022-05-17
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
CONTROL METHOD OF TILT ROTOR UNMANNED AERIAL VEHICLE, AND TILT ROTOR UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2021
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