The invention discloses a fixed-wing unmanned aerial vehicle. The fixed-wing unmanned aerial vehicle comprises a fuselage main body, and wings and a tail which are installed on the fuselage main body, wherein the tail comprises an empennage and a tail rod fixed between the fuselage main body and the empennage; the wings comprise middle-section wings, left-section wings and right-section wings; the middle-section wings are fixed on the fuselage main body, and the left-section wings and the right-section wings are detachably installed on the left sides and the right sides of the middle-section wings respectively. According to the fixed-wing unmanned aerial vehicle disclosed by the invention, the whole wings of relatively large sizes are split into three sections respectively, wherein the middle-section wings can be integrated with electronic circuit equipment such as flying and receiving equipment, without being disassembled from the fuselage main body. In a transportation process, the left-section wings and the right-section wings can be disassembled, so that the space is saved, and the transportation is convenient.


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    Titel :

    Fixed-wing unmanned aerial vehicle


    Beteiligte:
    YANG HUADONG (Autor:in) / WU QICAI (Autor:in) / ZHAO JIANG (Autor:in)

    Erscheinungsdatum :

    10.06.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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