The invention discloses a high-compactness single-engine unmanned tilt rotorcraft transmission system and an unmanned aerial vehicle, and relates to the field of tilt rotorcraft transmission. One end of the transmission mechanism is connected with the other end of the clutch, and the transmission mechanism is arranged in the height direction of the machine body; the input end of the speed change structure is connected with the other end of the transmission mechanism, and the speed change structure is arranged above the engine; the left rotor system and the right rotor system are respectively connected with the output end of the speed change structure; the transmission system solves the problem that due to a single-engine unmanned tilt rotorcraft transmission system, the gravity center of the whole rotorcraft is close to the rear, the weight of a balancing weight on the front portion of the rotorcraft body is reduced, the flying windward area of the rotorcraft body is reduced, and the effect of improving task loads and flying control performance of the whole rotorcraft is achieved.

    本发明公开了一种高紧凑单发无人倾转旋翼机传动系统及无人机,涉及倾转旋翼机传动领域,包括:离合器,一端与发动机的输出轴连接;传动机构,一端与离合器的另一端连接,传动机构沿机身的高度方向设置;变速结构,输入端与传动机构的另一端连接,变速结构设置在发动机的上方;左旋翼系统和右旋翼系统,分别与变速结构的输出端连接;该传动系统解决单发无人倾转旋翼机传动系统导致的整机重心靠后问题,减小机身前部配重块重量,降低机身飞行迎风面积,实现提升整机任务载荷和飞行控制性能的效果。


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    Titel :

    High-compactness single-engine unmanned tilt rotorcraft transmission system and unmanned aerial vehicle


    Weitere Titelangaben:

    一种高紧凑单发无人倾转旋翼机传动系统及无人机


    Beteiligte:
    XU ZHIXIONG (Autor:in) / ZHOU BO (Autor:in) / ZHANG LIAN (Autor:in)

    Erscheinungsdatum :

    2023-05-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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