The invention relates to a fixed-axis tilt-rotor aircraft, which belongs to the technical field of aircrafts, and comprises a fuselage, symmetrically arranged main wings are respectively arranged on two sides of the front part of the fuselage, a tilt shaft is arranged in the front part of the fuselage, the tilt shaft is fixedly connected with the fuselage, and two ends of the tilt shaft are respectively inserted into the main wings and are rotatably connected with the main wings; power cabins are respectively arranged on the main wings on the two sides and are in power connection with rotor wings, main wing tilting driving modules are fixedly mounted in the power cabins on the two sides, and the main wing tilting driving modules are moved out of the fuselage, so that the clear height in the cabin reaches the level of a traditional fixed-wing aircraft; and the direction response speed in the vertical take-off and landing state is improved.
本发明涉及一种定轴倾转旋翼飞行器,属于飞行器技术领域,包括机身,机身的前部两侧分别设有对称设置的主翼,机身前部内置有倾转轴,倾转轴与机身固定连接,倾转轴的两端分别插入主翼并与主翼可转动连接,两侧的主翼上分别设有动力舱,动力舱动力连接有旋翼,两侧的动力舱内固定安装有主翼倾转驱动模块,由于主翼倾转驱动模块移出机身,使机仓内部净高达到传统固定翼飞机水平,同时,由于左右机翼倾转既可以同步也可以差动,提高了垂直起降状态下方向响应速度。
Fixed-axis tilt-rotor aircraft
一种定轴倾转旋翼飞行器
2024-05-28
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |