The invention provides a plasma propulsion unmanned aerial vehicle. The plasma propulsion unmanned aerial vehicle comprises an unmanned aerial vehicle body, a high-voltage electrode propulsion device, a high-voltage power converter and an energy storage battery, the unmanned aerial vehicle body comprises a fuselage, wings, an empennage and a fuselage tail pipe, the wings are arranged on two sides of the fuselage, and the fuselage tail pipe is connected with the fuselage and the empennage; the high-voltage electrode propulsion device comprises a plurality of groups of electrode arrays and a mounting assembly, each group of electrode arrays comprises a plurality of pairs of electrode units which are arranged up and down, each pair of electrode units comprises a wire arranged at the front part and a wing-shaped strip arranged at the rear part, and the mounting assembly comprises a wing-shaped strip bracket, a wire bracket and a wing bracket; the high-voltage power converter and the energy storage battery are both arranged in the fuselage, the positive and negative electrodes of the input end of the high-voltage power converter are both connected with the energy storage battery, the positive electrode of the output end is connected with the wire, and the negative electrode of the output end is connected with the wing-shaped strip. The technical problem that an existing power propulsion type unmanned aerial vehicle is prone to causing noise pollution and combustion emission pollution can be solved.

    本发明提供了一种等离子推进无人机,包括无人机本体、高压电极推进装置、高压功率变换器和储能电池;无人机本体包括机身、机翼、尾翼和机身尾管,机翼设置于机身的两侧,机身尾管与机身和尾翼相连;高压电极推进装置包括多组电极阵列和安装组件,每组电极阵列包括多对呈上下排列的电极单元,每对电极单元包括设置于前部的导线和设置于后部的翼型长条,安装组件包括翼型长条支架、导线支架和机翼支架;高压功率变换器和储能电池均设置于机身的内部,高压功率变换器的输入端正负极均与储能电池相连,输出端正极与导线相连,输出端负极与翼型长条相连。本发明能够解决现有的动力推进型式的无人机容易造成噪声污染和燃烧排放物污染的技术问题。


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    Titel :

    Plasma propulsion unmanned aerial vehicle


    Weitere Titelangaben:

    一种等离子推进无人机


    Beteiligte:
    XU DONGDONG (Autor:in) / YANG FAYOU (Autor:in) / ZHANG HUA (Autor:in) / LI QING (Autor:in) / JIA ZHENNAN (Autor:in) / LI KAI (Autor:in) / HAO SHUAI (Autor:in)

    Erscheinungsdatum :

    2022-06-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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