The invention relates to a rotary support of a micro turbojet engine, and the rotary support comprises a pair of supporting side plates used for supporting a micro turbojet engine, and the micro turbojet engine is rotatably installed between the pair of supporting side plates through an engine clamping rotating device. A connecting cover plate used for being connected with bearing equipment is installed on the pair of supporting side plates above the micro turbojet engine. The rotary support further comprises a rotation driving device and a wireless controller used for controlling the rotation driving device; the wireless controller is in wireless connection with the rotation driving device, the deflection angle of the micro turbojet engine is accurately controlled by the wireless controller, and the jet direction of a tail jet nozzle of the micro turbojet engine is changed. The miniature turbojet engine is started in the horizontal state and works in the vertical direction, and the miniature turbojet engine is suitable for being fixed to the lower portion of the unmanned aerial vehicle to conduct aerial fire extinguishing, fire fighting and the like when serving as a core power device.

    本发明涉及一种微型涡喷发动机旋转支架,包括一对用于支撑微型涡喷发动机的支撑侧板,微型涡喷发动机通过发动机卡紧旋转装置可旋转的安装在一对所述的支撑侧板之间;用于连接承载设备的连接盖板安装在所述微型涡喷发动机上方的一对所述支撑侧板上;还包括旋转驱动装置和用于控制旋转驱动装置的无线控制器,所述的无线控制器与旋转驱动装置无线连接,无线控制器准确控制微型涡喷发动机的偏转角度,改变所述微型涡喷发动机尾喷喷口的喷射方向。本发明实现了微型涡喷发动机水平状态起动、垂直方向作业,适用于采用微型涡喷发动机作为核心动力装置时,将其固定在无人机下方,进行空中灭火、消防等。


    Access

    Download


    Export, share and cite



    Title :

    Rotary support of micro turbojet engine


    Additional title:

    微型涡喷发动机旋转支架


    Contributors:
    CAI YUANHU (author) / WEI JIAJIA (author) / YANG XIAOHANG (author)

    Publication date :

    2022-01-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Modeling of Micro Turbojet Engine

    Ashry, Mahmoud M. / Kamel, Mohamed K. / Shehata, Ahmed M. | AIAA | 2019


    MODELING OF MICRO TURBOJET ENGINE

    Ashry, Mahmoud M. / Kamel, Mohamed K. / Shehata, Ahmed M. | TIBKAT | 2019


    Turbojet engine

    Online Contents | 1996



    The Turbojet Engine

    Babu, V. | Springer Verlag | 2021