The invention discloses a petrol-electric hybrid five-rotor unmanned aerial vehicle and relates to an unmanned aerial vehicle (UAV). According to the invention, the problem that an existing UAV is short in cruising duration, low in load capacity and unstable in flight attitude is solved. The petrol-electric hybrid five-rotor UAV comprises a landing gear, a fuel tank, an engine, a main rotor, a power battery, a central plate and four auxiliary rotors, wherein the fuel tank is fixedly arranged at the middle of the landing gear, and the engine is fixed above the landing gear; the output shaft of the engine is used for driving the main rotor; a central plate is jointed between the main rotor and the engine through an engine support column; the power battery is arranged below the central plate; the fuel tank and the power battery are used for providing petrol-electric hybrid power to the engine; the four auxiliary rotors are uniformly distributed at the periphery of the central plate. The petrol-electric hybrid five-rotor UAV is long in cruising duration, high in load capacity and stable in flight attitude.


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    Titel :

    Petrol-electric hybrid five-rotor unmanned aerial vehicle


    Beteiligte:
    WANG ZHONGXIN (Autor:in) / LI YUANWEI (Autor:in) / SONG HAILONG (Autor:in)

    Erscheinungsdatum :

    30.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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