The invention discloses an aerofoil structure of a fixed-wing unmanned aerial vehicle. The aerofoil structure of a fixed-wing unmanned aerial vehicle comprises an aerofoil body. According to the invention, the upper surface of the aerofoil body is a convex surface curved upwards and the lower surface of the aerofoil body is a convex surface curved downward; the aerofoil body is formed by fixedly connecting a front aerofoil section located beside the wing root of the aerofoil body and a rear aerofoil section located beside the wing tail of the aerofoil body; vertical projection of the front aerofoil is rectangular while vertical projection of the rear aerofoil is trapezoidal; the angle range of a sweepback angle on a front edge of the rear aerofoil section is 7-10 degree and the angle range of a dihedral angle on the rear aerofoil section is 2-5 degrees. An unmanned aerial vehicle having the aerofoil structure of a fixed-wing unmanned aerial vehicle is characterized by being stable in flying and low in power consumption.


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    Titel :

    Aerofoil structure of fixed-wing unmanned aerial vehicle


    Beteiligte:
    LIN MEIDAN (Autor:in)

    Erscheinungsdatum :

    06.05.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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