The invention discloses an airframe structure and an unmanned aerial vehicle thereof, and belongs to the technical field of unmanned aerial vehicles. The number of the main wings is at least two, the two main wings are symmetrically arranged on the two sides of the main aircraft body, and propellers and motors for providing power for the propellers are arranged on the main wings; the upper vertical empennage is arranged at the upper end of the main machine body; the lower vertical empennage is arranged at the lower end of the host body; according to the airframe structure and the unmanned aerial vehicle, the characteristics of a fixed-wing unmanned aerial vehicle and the characteristics of a multi-rotor unmanned aerial vehicle can be considered, and the situation that the stability of the unmanned aerial vehicle is affected by turbulent flow generated by propellers of main wings of the unmanned aerial vehicle when the vertical flight state is converted into the horizontal flight state can be avoided.

    本申请公开了机体结构及其无人机,属于无人机技术领域,一种机体结构,包括:主机体;主机翼,至少设置有两个,两个主机翼对称设置在主机体两侧,且主机翼上设置有螺旋桨和给螺旋桨提供动力的电机;上垂直尾翼,设置在主机体上端;下垂直尾翼,设置在主机体下端;本申请提供了一种既能够兼顾固定翼无人机和多旋翼无人机特点,又能够避免从垂直飞行状态转化到水平飞行状态时,无人机的主机翼的螺旋桨产生的湍流、扰流对于无人机稳定性造成影响的机体结构及其无人机。


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    Titel :

    Airframe structure and unmanned aerial vehicle thereof


    Weitere Titelangaben:

    机体结构及其无人机


    Beteiligte:
    YANG WEI (Autor:in) / HE CHUNPENG (Autor:in) / ZHAO ZHILIANG (Autor:in) / ZHANG YI (Autor:in) / TAN XINGYANG (Autor:in) / CHEN LIANG (Autor:in) / DU RUI (Autor:in) / HU PENG (Autor:in) / LAI XIAOYUE (Autor:in)

    Erscheinungsdatum :

    2023-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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