The invention provides a full protection UAV (unmanned aerial vehicle) to improve the operational safety and portability of the UAV. The UAV comprises an UAV main body, a rotor wing connected with the UAV main body and a protective shell connected with the same, wherein the protective shell is a hollow closed shell, the protective shell comprises a hollow cavity, and the rotor wing is arranged in the hollow cavity. The rotor wing is arranged in the hollow cavity, so that the rotor wing can not contact with the human body, the operator can release or recover the UAV by hand, the operating efficiency of the rotor wing is improved, and the operating safety is greatly improved; the protective shell is the hollow closed shell, the hollow structure provides a lift force generating space for the rotor wing to guarantee the UAV to fly normally; the rotor wing is arrnaged in the protective shell connected with the UAV main body, the whole height of the UAV is reduced, so that the portability of the UAV is improved.


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    Titel :

    Full protection unmanned aerial vehicle


    Beteiligte:
    ZHANG TONG (Autor:in) / WANG MENGQIU (Autor:in) / WANG ZHAOZHE (Autor:in) / ZHANG XUYANG (Autor:in) / ZHANG GUANQUN (Autor:in) / GONG SHUANG (Autor:in) / ZHANG YALIN (Autor:in) / WANG JINGLONG (Autor:in) / LIU LIXIN (Autor:in)

    Erscheinungsdatum :

    17.02.2016


    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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