The invention discloses a helicopter wind tunnel test bed balance rotation calibration loading device, which comprises a test device, a tension fixed pulley block, a horizontal fixed pulley and a weight disc, wherein the test device comprises a device table, a torque balance, a rotor balance, a rotor shaft, a dynamic torque sensor, a brake and a brake support; the rotor balance is arranged on thedevice table, the torque balance is arranged on the rotor shaft, and the torque balance is connected with the rotor shaft through a diaphragm coupling; the rotor shaft penetrates through the device table and the rotor balance, and the upper end of the rotor shaft is connected with the brake through the dynamic torque sensor; the brake is connected with the rotor balance through the brake support;the tension fixed pulley block is arranged above the brake; the horizontal fixed pulley is arranged on the side of the brake; and the weight disc is arranged at the tail end of a pulley rope. By adopting the helicopter wind tunnel test bed balance rotation calibration loading device and the calibration loading method, rotor balance and torque balance calibration coefficients in a rotation state can be given.

    本发明公开了一种直升机风洞试验台天平旋转标定加载装置,包括试验装置,其包括装置台、扭矩天平、旋翼天平、旋翼轴、动态扭矩传感器、制动器和制动器支架;所述旋翼天平设置于装置台上,扭矩天平设置于旋翼轴上,扭矩天平与旋翼轴通过膜片联轴器连接;所述旋翼轴穿过装置台和旋翼天平,旋翼轴上端通过动态扭矩传感器与制动器连接;制动器通过制动器支架与旋翼天平连接;拉力定滑轮组,其设置于制动器的上方;水平定滑轮,其设置于制动器的侧方;砝码盘,其设置于滑轮绳的末端。采用本发明的直升机风洞试验台天平旋转标定加载装置及标定加载方法,能实现给出旋转状态下的旋翼天平、扭矩天平标定系数。


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    Title :

    Helicopter wind tunnel test bed balance rotation calibration loading device and calibration loading method


    Additional title:

    直升机风洞试验台天平旋转标定加载装置及标定加载方法


    Contributors:
    ZHANG XIN (author) / WANG CHANG (author) / MA SHUAI (author) / YIN XINFAN (author) / TANG MIN (author) / ZHANG WEIGUO (author) / ZHAO LIANGLIANG (author) / TIAN BIN (author) / PENG XIANMIN (author)

    Publication date :

    2020-11-20


    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 / G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE



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