A main shaft support is installed in an aircraft body, a main shaft is installed on the main shaft support through a main shaft bearing, the upper end of the main shaft is connected with a rotor wing head, a rotor wing assembly and a folding paddle assembly are installed on the rotor wing head in a staggered mode, and a swash plate assembly is installed at the upper end of the main shaft and located below the rotor wing head. The rotor wing push-pull rod assembly is connected above the swash plate assembly, the swash plate push-pull rod assembly is connected below the swash plate assembly, the rotor wing assembly is connected with the swash plate assembly through the rotor wing push-pull rod assembly, and the swash plate steering engine is installed on the main shaft support and connected with the swash plate assembly through the swash plate push-pull rod assembly. A back propeller assembly is installed on the back face of the aircraft body, and a direction steering engine assembly is installed on an empennage of the aircraft body. The aircraft is driven to take off by driving the folding paddles, the reverse torsional moment is offset through air, the structural design is compact, stability and cruising ability are high, taking off and landing are more stable, and safety is high.

    本发明公开了一种复合型旋翼无人机飞行器,其中飞行器主体内安装有主轴支架,主轴通过主轴轴承安装在主轴支架上,主轴上端与旋翼头相连,旋翼头上交错安装有旋翼组件和折叠桨组件,主轴上端且位于旋翼头下方安装有倾斜盘组件,倾斜盘组件上方连接有旋翼推拉杆组件、下方连接有倾斜盘推拉杆组件,旋翼组件通过旋翼推拉杆组件与倾斜盘组件相连,倾斜盘舵机安装在主轴支架上,倾斜盘舵机通过倾斜盘推拉杆组件与倾斜盘组件相连,飞行器主体的背面安装有背推桨组件,方向舵机组件安装设置在飞行器主体的尾翼处。本发明通过驱动折叠桨叶带动飞行器起飞,用空气抵消反扭力矩,结构设计紧凑,且稳定性和续航能力强,起落更加稳定,安全性高。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Composite rotor unmanned aerial vehicle aircraft


    Weitere Titelangaben:

    一种复合型旋翼无人机飞行器


    Beteiligte:
    BAO JINGYUN (Autor:in) / WANG WEI (Autor:in)

    Erscheinungsdatum :

    17.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



    Composite multi-rotor unmanned aerial vehicle

    LI LEI / YANG YANHENG | Europäisches Patentamt | 2022

    Freier Zugriff

    Unmanned aerial vehicle folding arm, four-rotor unmanned aerial vehicle and six-rotor unmanned aerial vehicle

    TANG HUIPING / CHEN QIDONG / ZHANG PENG et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Rotor unmanned aerial vehicle

    ZHU YUAN / WANG JIZHEN / BAI CHUNYU et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Unmanned aerial vehicle rotor assembly and unmanned aerial vehicle

    HUANG LI / ZHOU YUANLIN / FEI CHAO et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    MULTI-ROTOR UNMANNED AERIAL VEHICLE AND MULTI-ROTOR UNMANNED AERIAL VEHICLE SYSTEM

    CHEN TAO / ZHAI LIUYANG / CAI YONGWEI | Europäisches Patentamt | 2022

    Freier Zugriff