The invention discloses a rotor reaction torque balance wing and an aircraft. The rotor reaction torque balance wing is simple in structure and few in component, is mounted below the rotor on the premise of guaranteeing the stability of the gravity center of the aircraft, and can automatically eliminate the reaction torque effect on the flight device by the rotation of the rotor by utilizing the transverse acting force generated by the adjusted inclined pneumatic surface of the blade under the downward wind pressure effect of the rotor, so that the stability of the aircraft is improved. And the aim of balancing the reaction torque of the rotor wing can be achieved without designing a tail rotor or a tail jet device and the like. The two blades are arranged on the aircraft in a central symmetry mode, various kinds of force such as downward pressure and forward resistance generated by the two blades can be counteracted, the aircraft does not need to be subjected to additional posture adjustment, and driving is easier, more convenient and safer due to the fact that no additional acting force is generated. If the whole device adopts a motor as a driving source, the energy consumption can be reduced; the aircraft comprises the rotor reaction torque balance wing and has all the characteristics and advantages of the rotor reaction torque balance wing.
本发明公开了一种旋翼反扭矩平衡翼及飞行器。旋翼反扭矩平衡翼结构简单、部件少,在保障飞行器重心稳定的前提下,将其安装在旋翼下方,可以在旋翼向下风压的作用下,利用叶片的调节好的倾斜气动面产生的横向作用力自动消除旋翼旋转对飞行装置形成的反扭矩作用,无需设计尾桨或尾喷等装置,也可实现对旋翼反扭矩平衡的目的。两个叶片呈中心对称地布置在飞行器上,它们产生的下压力以及前进阻力等各种力可以互相抵消,飞行器无需为此作出额外的姿态调节,由于没有产生额外的作用力使得驾驶更简便安全。整套装置若采用电机作为驱动源,则可降低能耗;飞行器包含上述旋翼反扭矩平衡翼,具备上述旋翼反扭矩平衡翼的全部特点优势。
Rotor reaction torque balance wing and aircraft
旋翼反扭矩平衡翼及飞行器
2025-04-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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