The invention discloses an unmanned aerial vehicle, a control terminal, a rescue method and a rescue system. The unmanned aerial vehicle comprises a vehicle body; the at least two rotor wings are rotatably arranged on the aircraft body, the at least two rotor wings provide first thrust in the first direction when rotating in the forward direction, the at least two rotor wings provide second thrust in the second direction when rotating in the reverse direction, and the first direction is opposite to the second direction; wherein when the aircraft body is in a to-be-rescued attitude and the unmanned aerial vehicle can execute an aircraft rescuing operation, at least part of the at least two rotors can provide the second thrust in response to an aircraft rescuing control instruction so as to execute the aircraft rescuing operation.

    一种无人飞行器、控制终端、救机方法和救机系统,该无人飞行器包括机体;至少两个旋翼,可转动地设置在所述机体上,至少两个所述旋翼各自在正向旋转时提供沿第一方向的第一推力,至少两个所述旋翼各自在反向旋转时提供沿第二方向的第二推力,所述第一方向与所述第二方向相反;其中,当所述机体处于待救机姿态,并且所述无人飞行器能够执行救机操作时,至少两个所述旋翼中至少部分旋翼能够响应于救机控制指令提供所述第二推力,以执行救机操作。


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    Titel :

    Unmanned aerial vehicle, control terminal, rescue method and rescue system


    Weitere Titelangaben:

    无人飞行器、控制终端、救机方法和救机系统


    Beteiligte:
    LI LUOCHUAN (Autor:in) / DUAN WUYANG (Autor:in) / SHANG ZHIMENG (Autor:in) / LYU XIMIN (Autor:in)

    Erscheinungsdatum :

    13.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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