The invention discloses a fixed-wing unmanned aerial vehicle. The fixed-wing unmanned aerial vehicle comprises a fuselage, a pair of wings which is positioned on two sides of the fuselage and symmetrically arranged, and an empennage mechanism positioned on the rear part of the fuselage, wherein a pair of propellers is symmetrically arranged on the outer sides of the leading edges of the pair of wings, and a power driving device for providing power for the rotation of the propellers is arranged in the fuselage; the power driving device comprises a first driving motor, a second driving motor and a battery; a power arm of the first driving motor and a power arm of the second driving motor are respectively connected with different propellers, and the first driving motor and the second driving motor are connected in parallel with the battery. The fixed-wing unmanned aerial vehicle disclosed by the invention has the characteristics of low power, long flight time, convenience in disassembling and assembling, and stability in flight.


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    Titel :

    Fixed-wing unmanned aerial vehicle


    Beteiligte:
    LIN MEIDAN (Autor:in)

    Erscheinungsdatum :

    2015-04-29


    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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