The invention discloses a power rotor wing of an aircraft, the rotor wing is composed of at least two half-side hang gliders which are uniformly distributed along the circumference, the rotor wing is connected with a rotor wing pivot, and the rotor wing pivot is rotatably connected with an output shaft of a power motor. The unmanned aerial vehicle is simple in structure, the wide and thick hang gliders serve as the rotor wings to form large lift force, high-speed airflow generated by the centrifugal fan with higher efficiency is used for generating centrifugal force through rotation of the rotor wings, the high-speed airflow is sprayed out through the wingtips, the power is maximized relative to the force arm of a center shaft of the rotor wings, the rotor wings can be pushed to rotate only through small thrust, and the unmanned aerial vehicle can be driven to rotate. The overall efficiency is high; as the hang glider is wide in breadth, the rotation speed does not need to be very high when the hang glider serves as a rotor wing, the generated noise is low, and the load capacity is high.

    本发明公开了一种飞行器的动力旋翼,由至少两个沿圆周均布的半边滑翔翼构成旋翼,旋翼与旋翼中枢连接,旋翼中枢与动力马达输出轴旋转连接。本发明结构简单,用较为宽厚的滑翔翼作为旋翼形成较大升力,用效率更高的离心风机产生的高速气流在通过旋翼旋转产生离心力,高速气流通过翼尖喷出,动力相对于旋翼中轴的力臂已最大化,只需要很小的推力就可以推动旋翼旋转,整体效率高;由于滑翔翼幅面宽大,作为旋翼时旋转速度不需要很高,产生的噪音小,负载能力强。


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    Title :

    Power rotor wing of aircraft


    Additional title:

    一种飞行器的动力旋翼


    Contributors:
    XU HANG (author)

    Publication date :

    2025-04-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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