The invention discloses a ship-borne heavy oil composite wing unmanned aerial vehicle which comprises a vehicle body, wings, a horizontal tail wing, a vertical tail wing, a heavy oil engine, propulsion propellers, rotor electronic speed controllers, rotor motors and propellers. The wings are arranged on two sides of the fuselage; the horizontal tail wing and the vertical tail wing are arranged atthe tail of the vehicle body; the heavy oil engine is arranged at the tail of the vehicle body. The propeller is located at the tail of the fuselage. The helicopter is simple in structure and capableof vertically taking off and landing, and the endurance is obviously superior to that of helicopters.

    本发明公开了一种舰载重油复合翼无人机,包括机身、机翼、水平尾翼、垂直尾翼、重油发动机以及推进螺旋桨、旋翼电调、旋翼电机及螺旋桨;机翼设置在机身两侧,水平尾翼和垂直尾翼设置在机身尾部;重油发动机设置在机身内,螺旋桨位于机身尾部。本发明结构简单,可垂直起降,且航时明显优于直升机。


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    Titel :

    Ship-borne heavy oil composite wing unmanned aerial vehicle


    Weitere Titelangaben:

    一种舰载重油复合翼无人机


    Beteiligte:
    HOU LIYANG (Autor:in) / CHEN GUOQI (Autor:in)

    Erscheinungsdatum :

    2020-06-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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