The invention provides a helicopter transmission system coaxiality detection and adjustment device and method, the device comprises a main controller 10, a laser emitter 20 and a laser receiver CCD 30, the main controller 10 comprises a computer 11 and a control box 12, after a control instruction on the computer 11 is sent, the control instruction is directly transmitted to the control box 12 through a USB interface; the laser transmitter 20 comprises a first laser transmitter 21 and a second laser transmitter 22, the first laser transmitter 21 comprises a first laser transmitter 211, a first adjusting flange 212 and a positioning cylinder 213, and the second laser transmitter 22 comprises a second laser transmitter 221, a second adjusting flange 222 and a positioning cylinder 223; the laser transmitter 20 is installed on a simulation output shaft flange plate of an engine or a main speed reducer, and the positioning cylinder 223 and the output end of the engine or the main speed reducer are installed in a positioning fit mode.

    本申请提供一种直升机传动系统同轴度检测及调整装置和方法,所述装置包括主控制器10、激光发射器20、激光接收器CCD30,其中:所述主控制器10包括计算机11和控制箱12,计算机11上的控制指令发出后,控制指令通过USB接口直接传输到控制箱12;所述激光发射器20包括Ⅰ号激光发射器21和Ⅱ号激光发射器22,所述Ⅰ号激光发射器21包括第一激光发射器211和第一调节法兰212和定位圆柱体213,所述Ⅱ号激光发射器22包括第二激光发射器221和第二调节法兰222和定位圆柱体223;激光发射器20安装在发动机或主减速器模拟输出轴法兰盘上,定位圆柱体223与发动机或主减速器输出端定位配合安装。


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    Title :

    Helicopter transmission system coaxiality detection and adjustment device and method


    Additional title:

    一种直升机传动系统同轴度检测及调整装置和方法


    Contributors:
    ZHANG JIN (author) / ZHOU JUN (author) / DU YAWEI (author) / ZHANG LING (author) / GAN YANLAN (author) / WAN YONG (author) / GAN HAOYU (author)

    Publication date :

    2024-12-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / 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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