The invention relates to the technical field of unmanned aerial vehicles and discloses a vertical take-off and landing tandem wing unmanned aerial vehicle which comprises a vehicle body, front wings,rear wings, a propeller assembly and a vertical fin. The propeller assembly comprises a propelling propeller assembly and a take-off and landing propeller assembly; the propelling propeller assembly is arranged at a tail of the vehicle body; a reinforcing assembly is arranged at vehicle body, the reinforcing assembly comprises two longitudinal rods which are symmetrically distributed left and right relative to the center of the vehicle body, and a transverse rod between the two longitudinal rods; the take-off and landing propeller assembly is arranged at a joint of the longitudinal rods and the transverse rod; the front end of each longitudinal rod extends to the bottom of each front wing; the front part of each longitudinal rod is connected with the front wings; the rear end of each longitudinal rod extends to the bottom of each rear wing; and the rear portion of each longitudinal rod is connected with each rear wing, a front wing reinforcing rod is arranged in the front wing, the front portion of the longitudinal rod is connected with the front wing reinforcing rod, the rear wing reinforcing rod is arranged in each rear wing, the rear portion of each longitudinal rod is connectedwith the rear wing reinforcing rod, rigidity of the unmanned aerial vehicle is sufficient, falling resistance is good, losses after falling are greatly reduced, and a cruising ability is greatly improved.

    本发明涉及无人机技术领域,具体涉及垂直起降的串列翼无人机,包括机体、前翼、后翼、螺旋桨组件及垂尾,螺旋桨组件包括推进螺旋桨组件、起降螺旋桨组件,推进螺旋桨组件设置在机体尾部,机体处设有加强组件,加强组件包括两个关于机体中心左右对称分布的纵向杆、两纵向杆之间的横向杆,起降螺旋桨组件设置在纵向杆上与横向杆相接处,纵向杆前端延伸至前翼的底部处,纵向杆前部与前翼连接,纵向杆后端延伸至后翼的底部处,纵向杆后部与后翼连接,前翼内设有前翼加强杆,纵向杆前部与前翼加强杆连接,后翼内设有后翼加强杆,纵向杆的后部与后翼加强杆连接,无人机的刚性足,抗摔性好,较大幅度降低摔机后的损失,续航能力较大提升。


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    Titel :

    Vertical take-off and landing tandem wing unmanned aerial vehicle


    Weitere Titelangaben:

    垂直起降的串列翼无人机


    Beteiligte:
    LIU YANG (Autor:in) / JU WEIJIE (Autor:in) / JU ZHUQING (Autor:in)

    Erscheinungsdatum :

    2020-08-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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