The invention provides a vertical take-off and landing unmanned aerial vehicle which comprises a frame type fuselage. The outer contour of the frame type fuselage is circular. multiple turbojet engines are distributed on the peripheral side of the frame type fuselage at equal intervals; the vertical take-off and landing unmanned aerial vehicle is large in load, reliable in high-altitude take-off and landing performance and high in take-off and landing safety.

    本发明提供了一种垂直起降无人机,该垂直起降无人机包括:框架式机身,所述框架式机身的外轮廓呈圆形;多个涡喷发动机,多个所述涡喷发动机等间距分布在所述框架式机身的周侧;货运吊舱,连接于所述框架式机身,位于所述框架式机身的中部,该垂直起降无人机具载重大、高海拔起降性可靠、起降安全性高。


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    Titel :

    Vertical take-off and landing unmanned aerial vehicle


    Weitere Titelangaben:

    垂直起降无人机


    Beteiligte:
    ZHANG LIHUI (Autor:in) / ZHANG YONG (Autor:in)

    Erscheinungsdatum :

    2021-08-24


    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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