The invention provides a rotor-free unmanned aerial vehicle which comprises a vehicle body and injection devices distributed on the two sides of the vehicle body, and a power system, a gas compressor and a gas mixing chamber are arranged in the vehicle body; the power system is located in the center of the machine body, an air inlet faces upwards, and power is input into the air compressor. The gas compressor sucks gas into the gas mixing chamber through power provided by the power system; and the gas mixing chamber is used for guiding the gas to the injection device. A traditional rotary wing type vertical take-off and landing power mode is abandoned, vertical take-off and landing are achieved through the engine with the high thrust-weight ratio, and the technical performance of the unmanned aerial vehicle and the processing capacity of civil and commercial application scenes are emphasized.

    本发明提供了一种无旋翼无人机,包括机身以及分布在机身两侧的喷射装置,所述机身内设置有动力系统、压气机和气体混合室;所述的动力系统位于机体中央,进气口朝上,将动力输入压气机;所述的压气机,通过动力系统提供的动力将气体吸入至气体混合室;所述的气体混合室将气体导流至喷射装置。本发明摒除了传统的旋翼式垂直起降动力模式,采用推重比高的发动机来实现垂直起降,更加侧重无人机的技术性能及民用、商用应用场景的处理能力。


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    Titel :

    Rotor-free unmanned aerial vehicle


    Weitere Titelangaben:

    无旋翼无人机


    Beteiligte:
    XU JUNFEI (Autor:in) / LI XIAOGUANG (Autor:in) / HUAN PING (Autor:in)

    Erscheinungsdatum :

    04.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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