The invention discloses a tilting rotor system with variable wings and rotor nacels.The tilting rotor system comprises a tilting rotor aircraft, a first tilting device, a second tilting device, a third tilting device, a fourth tilting device, a fourth tilting device, a fifth tilting device, a sixth tilting device, a fifth tilting device and a sixth tilting device, the second tilting device is arranged on a connecting shaft of a wing and a rotor nacelle of the tilting rotor aircraft; the first tilting device is used for driving the wings to rotate relative to the fuselage, and the second tilting device is used for driving the rotor wing nacelles to rotate relative to the wings. By means of the first tilting devices on the connecting shafts of the fuselage and the wings and the second tilting devices on the connecting shafts of the wings and the rotor nacelles, independent control over the wings and the rotor nacelles is achieved, and then accurate control over lift force and thrust of the whole aircraft in the tilting transition state is achieved.
本发明公开一种可变机翼及旋翼短舱的倾转旋翼系统及其控制方法,所述倾转旋翼系统包括倾转旋翼飞行器,设置在倾转旋翼飞行器的机身与机翼的连接轴上的第一倾转装置,及设置在倾转旋翼飞行器的机翼与旋翼短舱的连接轴上的第二倾转装置;所述第一倾转装置用于带动所述机翼相对于所述机身转动,所述第二倾转装置用于带动所述旋翼短舱相对于所述机翼转动。本发明通过在机身与机翼的连接轴上的第一倾转装置,在机翼与旋翼短舱的连接轴上的第二倾转装置,实现机翼及旋翼短舱的单独控制,进而实现倾转过渡状态全机升力和推力的精准控制。
Tilt rotor system with variable wings and rotor nacelles and control method of tilt rotor system
一种可变机翼及旋翼短舱的倾转旋翼系统及其控制方法
29.08.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |