The invention discloses a plasma vertical take-off and landing unmanned aerial vehicle which comprises an unmanned aerial vehicle center structural body, plasma propellers are fixedly installed on the two sides of the unmanned aerial vehicle center structural body and supported by propeller supporting frames, and an undercarriage is arranged below the unmanned aerial vehicle center structural body. According to the plasma vertical take-off and landing unmanned aerial vehicle, the problems of noise pollution and combustion emission pollution of a traditional power propulsion unmanned aerial vehicle can be solved, and the plasma vertical take-off and landing unmanned aerial vehicle is more suitable for military low-altitude reconnaissance activities and civil low-altitude operation.

    本发明公开了一种等离子垂直起降无人机,包括无人机中心结构体,所述无人机中心结构体的两侧安装固定有等离子推进器,所述等离子推进器由推进器支撑架支撑,所述无人机中心结构体的下方设有起落架。本发明采用上述的一种等离子垂直起降无人机,可以解决传统动力推进无人机噪声污染和燃烧排放物污染的问题,更加适用于军事方面低空侦察活动以及民用低空作业。


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    Titel :

    Plasma vertical take-off and landing unmanned aerial vehicle


    Weitere Titelangaben:

    一种等离子垂直起降无人机


    Beteiligte:
    HUO MINGYING (Autor:in) / YING YULONG (Autor:in) / LIN TONG (Autor:in) / QI NAIMING (Autor:in) / LI ZHONGJIAN (Autor:in) / YANG DIANLIANG (Autor:in)

    Erscheinungsdatum :

    24.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen



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