The invention discloses an unmanned aerial vehicle group launching mechanism which comprises a motor, a speed reduction system, a launching mechanism, a conveying mechanism and a transmission assembly, wherein the motor serves as a power source and provides power for mechanism operation, and a motor output shaft of the motor is connected with the speed reduction system; the speed reduction system is used for reducing the speed and increasing the torque of the input power and driving the launching mechanism to work, and the speed reduction system is connected with the transmission assembly through a first bevel gear; the launching mechanism is used for launching the unmanned aerial vehicle; the conveying mechanism is used for conveying the unmanned aerial vehicle into the launching mechanism; the transmission assembly is used for transmitting power to the conveying mechanism; and the motor, the launching mechanism and the transmission assembly are all installed on a carrying disc of the conveying mechanism. According to the unmanned aerial vehicle group launching mechanism, a mechanical cluster launching system is adopted, compared with a common single launching technology, high-frequency, rapid and automatic launching of folding wing unmanned aerial vehicles can be achieved, and compared with a common gunpowder actuation type cluster launching technology, the unmanned aerial vehicle group launching mechanism is small in impact on the unmanned aerial vehicles, light in damage and beneficial to recycling of the unmanned aerial vehicles.

    本发明公开了一种无人机群发机构,包括电机,作为动力源,为机构运行提供动力,所述电机的电机输出轴连接减速系统;减速系统,用于对输入的动力进行减速增矩并带动发射机构工作,所述减速系统通过第一锥形齿轮与传动组件相连;发射机构,用于发射无人机;输送机构,用于将无人机输送到所述发射机构内;传动组件,用于将动力传递至输送机构;所述电机、发射机构和传动组件均安装在所述输送机构的载盘上。该无人机群发机构,采用机械式集群发射系统,与常见的单次发射技术相比,本发明可以实现折叠翼无人机高频率、快速、自动发射,与一般的火药作动式集群发射技术相比,本发明对无人机冲击小,损伤轻,有利于无人机的回收使用。


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    Title :

    Unmanned aerial vehicle group launching mechanism


    Additional title:

    一种无人机群发机构


    Contributors:
    PANG HUAN (author) / WANG DAOCHENG (author) / LIU JINGYI (author) / SHI DONGYANG (author)

    Publication date :

    2021-07-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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