The invention discloses a canard tail seat type unmanned aerial vehicle. The unmanned aerial vehicle comprises a fuselage, wings, canards, a power assembly and aileron assemblies. Each aileron assembly comprises an aileron, a cicada wing, a second driving assembly and a third driving assembly, the two aileron assemblies are connected with the two wings respectively, for any pair of aileron assembly and wing, one end of the aileron is rotationally connected with the rear edge of the wing, the second driving assembly is used for driving the aileron to swing, the cicada wings are in sliding connection with the aileron, the third driving assembly is used for driving the cicada wings overlapped with the aileron to extend out of the rear edge of the aileron, and the third driving assembly is further used for driving the cicada wings to retract to the position overlapped with the aileron from the rear edge of the aileron. The canard tail seat type unmanned aerial vehicle can provide larger steering effect in the vertical take-off and landing state, the unnecessary lift force is offset, and meanwhile the steering effect in the level flight cruise state is not affected.

    本发明公开了一种鸭翼尾座式无人机,包括机身、机翼、鸭翼、动力组件和副翼组件。副翼组件包括副翼、蝉翼、第二驱动组件和第三驱动组件,副翼组件设有两组,两组副翼组件分别与两个机翼连接,其中,对于任意一对的副翼组件和机翼:副翼的一端与机翼的后缘转动连接,第二驱动组件用于驱使副翼摆动,蝉翼与副翼滑动连接,第三驱动组件用于驱使与副翼重叠的蝉翼从副翼的后缘伸出,第三驱动组件还用于驱使蝉翼从副翼的后缘缩回至与副翼重叠的位置。本发明的鸭翼尾座式无人机能够在垂直起降状态提供更大的舵效,抵消了不必要的升力,同时不影响平飞巡航状态的舵效。


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    Title :

    Canard tail seat type unmanned aerial vehicle


    Additional title:

    鸭翼尾座式无人机


    Contributors:
    WU MENGFEI (author) / YIN YUCHEN (author) / CHEN XUANWU (author) / LIANG YU (author) / LIU YIJUN (author) / SHAN XIAOWEN (author)

    Publication date :

    2021-12-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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