The invention discloses an unmanned helicopter blade dynamic balance calibration system and calibration method. The unmanned helicopter blade dynamic balance calibration system comprises an unmanned helicopter blade mechanism, a laser range finder and a ground control station. According to the unmanned helicopter blade dynamic balance calibration system and calibration method disclosed by the invention, dynamic data of blades are acquired through the laser range finder, so that the data acquisition is safer and the accuracy is high; compared with a stroboscope method, the system is more economical and simple to operate; and after the collected data are coded, the currently collected data can be displayed in real time, and by means of an expert system of a ground control station, the qualification can be analyzed and judged, and the adjustment length of a paddle variable-pitch pull rod can be accurately indicated.

    本发明公开了一种无人直升机桨叶动平衡标定系统及标定方法,包括无人直升机桨叶机构、激光测距仪及地面控制站。本发明公开的一种无人直升机桨叶动平衡标定系统及标定方法,通过激光测距仪采集桨叶的动态数据,数据的获取更加安全、精准度高;而较频闪仪法获取数据更加经济、操作简单;并且将采集的数据通过编码后,可以实时的显示当前采集的数据,并且依靠地面控制站的专家系统,可以分析和判断合格性,精准指示桨叶变距拉杆的调整长度。


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    Title :

    Unmanned helicopter blade dynamic balance calibration system and calibration method


    Additional title:

    无人直升机桨叶动平衡标定系统及标定方法


    Contributors:

    Publication date :

    2020-12-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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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