The invention relates to the technical field of tilt rotors, in particular to a self-sustaining tilt rotor and an aircraft with the same. The self-sustaining type tilting rotor wing comprises a wing body, one end of the wing body is provided with a rotary connecting piece, and the rotary connecting piece is suitable for being rotationally connected with an aircraft body; and the connecting pieces are installed on the two sides of the wing body correspondingly, the connecting pieces extend in the direction away from the wing body, and rotor wing bodies are installed on the connecting pieces. According to the self-sustaining tilting rotor provided by the invention, different rotor bodies are directly controlled to operate at different rotating speeds, so that take-off, landing and advancing of an aircraft body are realized. The self-sustaining tilting rotor wing is simple in overall structure, pitching and yawing operation can be achieved by changing the rotating speed of the rotor wing body when an aircraft takes off and flatly flies, a tilting driving shaft and a corresponding driving power device are not needed to control rotation of the wing body, and the power utilization rate of the aircraft can be greatly increased.
本发明涉及倾转旋翼技术领域,具体涉及一种自持式倾转旋翼及具有其的航空器。自持式倾转旋翼,包括:机翼本体,其一端设置有转动连接件,转动连接件适于与航空器本体转动连接;一对连接件,分别安装在机翼本体两侧,连接件朝向远离机翼本体的方向延伸,连接件上安装有旋翼本体。本发明提供的自持式倾转旋翼,直接控制不同旋翼本体在不同转速下运行,来实现航空器本体的起飞、降落和前进。自持式倾转旋翼整体结构简单,航空器起飞、平飞时俯仰和偏航操纵可以由改变旋翼本体转速来实现,不需要倾转驱动轴和相应的驱动动力装置来控制机翼本体转动,能够大大提升航空器的动力功率利用率。
Self-sustaining type tilting rotor wing and aircraft with self-sustaining type tilting rotor wing
一种自持式倾转旋翼及具有其的航空器
2023-08-29
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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