The invention discloses a helicopter rotor wing driving structure which comprises a fuselage body with a shaft rod at the top end, at least one power main rotor wing group is arranged on the shaft rod, and the power main rotor wing group comprises main rotor wings which are arranged on the two sides of the shaft rod and correspond to each other. The propellers are arranged on the two sides of the shaft rod and correspond to each other, the propellers and the main rotor wings are located on the same horizontal plane and are correspondingly arranged at right-angle intervals, and the propellers are used for pushing the main rotor wings to rotate; therefore, the main rotor wings are directly driven by the propellers to generate rising buoyancy, the problems of an existing helicopter in the aspects of control, noise, air pollution, safety, repair, maintenance, energy consumption and the like can be solved, energy in flight can be used for generating electricity, and the endurance mileage can be effectively increased by recycling and storing the electricity; the problems that an existing helicopter driving device is complex, heavy and insufficient in power supply are solved.

    本发明公开了一种直升机旋翼驱动结构,其包括有一顶端设有轴杆的机身本体,所述轴杆上设置有至少一动力主旋翼组,所述动力主旋翼组包括有组设在所述轴杆的两侧且相互对应的主旋翼,及设置在所述轴杆的两侧且相互对应的推进器,所述推进器与所述主旋翼在同一水平面上并呈直角间隔对应设置,所述推进器用于推动所述主旋翼旋转;由此,通过所述推进器直接驱动所述主旋翼产生上升浮力,可改善现有直升机在操控、噪音、空气污染、安全、维修、保养、耗能等方面的问题,并能利用飞行中的能量发电并回收存储以有效提升续航里程,以解决现有直升机驱动装置复杂笨重和电力供应不足的问题。


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    Titel :

    Helicopter rotor driving structure


    Weitere Titelangaben:

    直升机旋翼驱动结构


    Beteiligte:
    LI QIUYAN (Autor:in)

    Erscheinungsdatum :

    2023-08-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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