The invention discloses a rotary outer wing vertical take-off and landing high-speed cruise fixed wing unmanned aerial vehicle. A undercarriage is fixed to the bottom of a fuselage, a vertical tail and a horizontal tail are fixed to the tail of the fuselage, and a nose propeller is connected to the head of the fuselage through a first motor; a duct penetrates through the position, close to the joint of the horizontal tail and the fuselage, of the fuselage, and a duct propeller is connected into the duct through a second motor; rotary outer wing structures are symmetrically fixed on two sides of the fuselage; the controller is in telecommunication connection with the rotary outer wing structure, during vertical take-off and landing, the controller controls the rotary outer wing structure to be in a form mode of disclosing lift force, and during level flight cruise, the controller controls the rotary outer wing structure to be in a form mode of disclosing level flight cruise power. The invention discloses the rotating outer wing vertical take-off and landing high-speed cruising fixed wing unmanned aerial vehicle, which has vertical take-off and landing and high-speed cruising performance, overcomes the limitation of mode switching difficulty of the unmanned aerial vehicle, and brings greater benefits.

    本发明公开了一种旋转外翼垂直起降高速巡航固定翼无人机,机身的底部固定有起落架,尾部分别固定有垂尾和平尾,头部通过第一电机连接有机头螺旋桨;机身靠近平尾与机身的连接处贯通有涵道,且涵道内通过第二电机连接有涵道螺旋桨;机身的两侧对称固定有旋转外翼机翼结构;控制器电信连接旋转外翼机翼结构,当垂直起降时,控制器控制旋转外翼机翼结构为公开升力的形态模式,当平飞巡航时,控制器控制旋转外翼机翼结构为公开平飞巡航动力的形态模式。本发明公开了一种旋转外翼垂直起降高速巡航固定翼无人机,具有垂直起降、高速巡航性能的同时,克服上述无人机在模式切换困难的局限性,带来更大效益。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotary outer wing vertical take-off and landing high-speed cruise fixed wing unmanned aerial vehicle


    Weitere Titelangaben:

    一种旋转外翼垂直起降高速巡航固定翼无人机


    Beteiligte:
    YUAN CHANGSHENG (Autor:in) / GUO YINGNAN (Autor:in) / GUO QING (Autor:in) / LIAO TIEJUN (Autor:in) / ZHAO TAO (Autor:in) / YANG YU (Autor:in) / ZHOU ZHENG (Autor:in) / FENG LISHUANG (Autor:in) / WANG QIANG (Autor:in)

    Erscheinungsdatum :

    03.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Vertical take-off and landing fixed-wing unmanned aerial vehicle

    TIAN YU | Europäisches Patentamt | 2020

    Freier Zugriff

    Vertical take-off and landing fixed-wing unmanned aerial vehicle

    SHI YONGKANG / WU HAO / LI PENG | Europäisches Patentamt | 2022

    Freier Zugriff

    Vertical take-off and landing fixed-wing unmanned aerial vehicle

    SUN WEI | Europäisches Patentamt | 2023

    Freier Zugriff

    Fixed-wing vertical take-off and landing unmanned aerial vehicle

    LIANG YU / SHAN XIAOWEN | Europäisches Patentamt | 2020

    Freier Zugriff

    Modularized vertical take-off and landing fixed-wing unmanned aerial vehicle

    WANG FANG / XU AN'AN | Europäisches Patentamt | 2021

    Freier Zugriff