The invention discloses a coaxial contra-rotating jet propeller in the technical field of unmanned aerial vehicles. The coaxial contra-rotating jet propeller is characterized by comprising a thrust system, the thrust system comprises a front fairing, a front propeller arranged at the rear end of the front fairing, a rear propeller arranged at the rear end of the front propeller, a main bearing arranged at the rear end of the rear propeller and a reversing gear set connected with the main bearing. The front paddle shaft drives the front paddle and the driving gear to rotate, the driving gear drives the steering gear to rotate, the steering gear drives the driven gear to rotate, the driven gear drives the rear paddle shaft to rotate, and the rear paddle shaft drives the rear paddle to rotate. Through cooperative use of the single motor and the steering gear set, the two propellers rotating in the opposite directions rotate at the same time, the contra-rotating propellers can automatically balance the torque, the torque shown outwards is balanced, induced resistance can be reduced, and efficiency is improved.

    本发明公开了无人机技术领域的一种同轴对转喷气推进器,其特征在于:包括:推力系统,所述推力系统包括前整流罩、设置在所述前整流罩后端的前桨、设置在所述前桨后端的后桨、设置在所述后桨后端的主轴承、与所述主轴承相连接的换向齿轮组,本发明通过电机上的输出轴配合联轴器带动前桨轴旋转,通过前桨轴带动前桨和主动齿轮旋转,通过主动齿轮带动转向齿轮旋转,通过转向齿轮带动从动齿轮旋转,通过从动齿轮带动后桨轴旋转,通过后桨轴带动后桨旋转,通过单电机与转向齿轮组的配合使用同时两个旋转方向相反的螺旋桨旋转,对转桨会自动平衡扭矩,对外表现出的扭矩平衡,且能够减少诱导阻力,提高效率。


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    Titel :

    Coaxial contra-rotating jet propeller


    Weitere Titelangaben:

    一种同轴对转喷气推进器


    Beteiligte:
    HE ZHIWEI (Autor:in) / ZHU ZHAOJUN (Autor:in) / ZHANG HELEI (Autor:in) / MA YAOLI (Autor:in) / SHAN CHENCHEN (Autor:in) / ZHANG XIANG (Autor:in) / HAN FEIFEI (Autor:in)

    Erscheinungsdatum :

    2023-03-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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