The invention provides a plasma propulsion ultra-silence flying robot system and a power combination control method, relates to the technical field of plasma propulsion aircrafts, and designs a flying robot of a novel plasma propulsion device with a high thrust-weight ratio. The technical problem that in the prior art, when propellers or engine blades adopted by aircrafts in a traditional propulsion mode rotate, inherent noise is still difficult to eliminate is solved. A flight control module of the system is used for receiving a flight control instruction transmitted by an upper computer; and the electrical module controls the plasma propulsion unit according to the flight control signal, so that the plasma propulsion unit generates plasma wind. According to the flying robot, the number of the needed plasma propelling units can be adjusted at will according to the flight mission requirement, the power layout of the plasma propelling units on the floating body can be conveniently changed, and therefore the whole robot obtains different maneuvering flight performance, and meanwhile ultra-silence long-endurance flight can be achieved under the condition that extra mechanical noise is not generated.

    本发明提供了等离子推进的超静音飞行机器人系统及动力组合控制方法,涉及等离子推进飞行器技术领域,设计了一种具有较高推重比的新型等离子推进装置的飞行机器人,解决了现有技术中存在的传统推进方式飞机采用的螺旋桨或引擎叶片转动时,固有的噪声仍然难以消除的技术问题。该系统的飞行控制模块用于接收上位机传送的飞行控制指令;电气模块根据飞行控制信号对等离子推进单元进行控制,从而使得等离子推进单元产生等离子风。该飞行机器人可根据飞行任务需求任意调整所需等离子推进单元的数量,较为便捷的改变等离子推进单元在浮空体上的动力布局,从而使整机获得不同的机动飞行性能,同时可以在不产生额外机械噪音的情况下实现超静音长续航飞行。


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    Titel :

    Plasma-propelled ultra-silence flying robot system and power combination control method


    Weitere Titelangaben:

    等离子推进的超静音飞行机器人系统及动力组合控制方法


    Beteiligte:
    ZHANG YIXIN (Autor:in) / ZHANG JIAWEI (Autor:in) / WANG ZIHAN (Autor:in) / LI ZHIJUN (Autor:in) / FAN XUANLIN (Autor:in) / WANG SHAOPING (Autor:in) / MIAO YINAN (Autor:in) / ZHAO ZHENG (Autor:in) / LIU CHENGXIN (Autor:in)

    Erscheinungsdatum :

    21.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / 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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