The invention relates to a vector thrust type unmanned aerial vehicle. The vector thrust type unmanned aerial vehicle comprises a propeller, an aircraft body, wings and empennages; the propeller is coaxially mounted at the front end of the longitudinal axis of the aircraft body; the wings are symmetrically mounted on two sides of the middle of the aircraft body; the empennages are symmetrically mounted on two sides of the tail of the aircraft body; a vector thrust device is mounted at the tail of the longitudinal axis of the aircraft body and comprises a motor and a spray pipe; the motor is mounted inside the aircraft body; the front end of the spray pipe is connected with the motor; and the tail end of the spray pipe extends out of the tail end of the aircraft body. The vector thrust typeunmanned aerial vehicle is scientific in design, reasonable in structure, high in controllability, high in takeoff and landing speed, good in safety, capable of guaranteeing maneuvering flight undera low-speed and large-attack-angle state, small in size, light in weight and good in maneuvering performance; and the maneuverability of the unmanned aerial vehicle is effectively improved; the sliding distance of the unmanned aerial vehicle in a takeoff and landing processes can be shortened.

    本发明涉及一种矢量推力型无人机,包括螺旋桨、机身、机翼以及尾翼,螺旋桨同轴安装在机身纵轴前端,机身中部两侧对称安装机翼,机身尾部两侧对称安装有尾翼,所述机身纵轴尾部安装有一矢量推力装置,该矢量推力装置包括电动机和喷管,所述电动机安装在机身内部,喷管前端连接电动机,喷管尾端伸出机身尾端。本发明设计科学、结构合理、可控性强、起落速度快、安全性好,可以保证在无人机作低速、大攻角状态机动飞行,体积小,质量轻,机动性能好,不仅有效提升无人机的机动性,而且可以缩短无人机起、落过程的滑跑距离。


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    Titel :

    Vector thrust type unmanned aerial vehicle


    Weitere Titelangaben:

    矢量推力型无人机


    Beteiligte:
    CHENG YONGJUN (Autor:in)

    Erscheinungsdatum :

    26.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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