The invention relates to the technical field of unmanned aerial vehicles, and discloses a barrel-shot coaxial dual-rotor unmanned aerial vehicle, the barrel-shot coaxial dual-rotor unmanned aerial vehicle comprises a launching part and a flying part, the launching part comprises a launching angle adjusting mechanism, a launching force adjusting mechanism, a position guiding and deviation preventing mechanism and a position locking mechanism, the launching force adjusting mechanism is movably mounted on the surface of the launching angle adjusting mechanism, and the position locking mechanism is movably mounted on the surface of the launching angle adjusting mechanism. The guide deviation preventing mechanism is fixedly installed in the launching force adjusting mechanism, the locking mechanism is installed in the guide deviation preventing mechanism, the flying part comprises a deviation preventing protection mechanism and a rotor wing transmission mechanism, and the rotor wing transmission mechanism is installed in the deviation preventing protection mechanism. According to the cylindrical shooting coaxial dual-rotor unmanned aerial vehicle, it is guaranteed that the flying part is pushed to pop out through mechanical thrust generated by the shooting strength adjusting mechanism in the use process, and compared with traditional medium shooting such as gas or gunpowder, stable storage and transportation are guaranteed, and the shooting characteristics such as flame light, shock waves and noise in the shooting process are reduced.

    本发明涉及无人机技术领域,且公开了一种筒射共轴双旋翼无人机,包括:发射部和飞行部,所述发射部包括发射角调整机构、发射力度调节机构、导位防偏机构和锁位机构,所述发射力度调节机构活动安装在发射角调整机构的表面,所述导位防偏机构固定安装在发射力度调节机构的内部,所述锁位机构安装在导位防偏机构的内部,所述飞行部包括防偏防护机构和旋翼传动机构,所述旋翼传动机构安装在防偏防护机构的内部。该筒射共轴双旋翼无人机,保障在使用时通过发射力度调节机构产生的机械推力推动飞行部弹出,相对于传统的缩气体或火药等介质发射,保障了稳定贮存与运输,降低了发射时的火光、冲击波和噪声等发射特征。


    Access

    Download


    Export, share and cite



    Title :

    Cylinder-launched coaxial dual-rotor unmanned aerial vehicle


    Additional title:

    一种筒射共轴双旋翼无人机


    Contributors:
    MA TONGLING (author) / WANG LIGUO (author) / GUAN XIAOLE (author) / CHAI XIYUAN (author) / HAN XUEMIN (author) / WANG ZEYU (author) / WANG XINWEI (author) / WANG QINGBEI (author) / LI ZIHAN (author) / ZHANG FAN (author)

    Publication date :

    2025-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



    Coaxial dual-rotor unmanned aerial vehicle

    YANG PENG / MA BIN | European Patent Office | 2021

    Free access

    Coaxial dual-rotor unmanned aerial vehicle

    LI JUN / HOU SHANCHUAN / ZENG LIFANG et al. | European Patent Office | 2025

    Free access

    Coaxial dual-rotor unmanned aerial vehicle

    WANG YULIN / DONG BIN / LI DONGDA | European Patent Office | 2022

    Free access

    Coaxial dual-rotor unmanned aerial vehicle

    LIU BIAO / WANG ZHIGANG / LI YIBO et al. | European Patent Office | 2022

    Free access

    COAXIAL DUAL-ROTOR UNMANNED AERIAL VEHICLE

    WANG YULIN / DONG BIN / LI DONGDA | European Patent Office | 2024

    Free access