The invention discloses a traction unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles, the traction unmanned aerial vehicle comprises an unmanned aerial vehicle structure, a power energy system is arranged at the lower end of the unmanned aerial vehicle structure, an avionics flight control system is arranged at the upper end of the unmanned aerial vehicle structure, the power energy system provides energy for the avionics flight control system, and the avionics flight control system drives the unmanned aerial vehicle to operate. The traction unmanned aerial vehicle has the advantages of being large in traction force, high in energy efficiency, high in safety, convenient to use and wide in application.

    本发明公开了一种牵引无人机,属于无人机技术领域,包括无人机结构,无人机结构的下端设置有动力能源系统,无人机结构的上端设置有航电飞控系统,动力能源系统给航电飞控系统提供能源,航电飞控系统驱动无人机运行。本发明一种牵引无人机具有牵引力大,能效高、安全性高、使用方便、应用广的特点。


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    Titel :

    Traction unmanned aerial vehicle


    Weitere Titelangaben:

    一种牵引无人机


    Beteiligte:
    WANG QIANG (Autor:in) / ZHU JIQUAN (Autor:in) / TAO ZHIJIA (Autor:in)

    Erscheinungsdatum :

    13.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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