The invention relates to an aircraft rotor test device. The aircraft rotor test equipment comprises a test bench, an upper rotor test device and a lower rotor test device, wherein the upper rotor test device and the lower rotor test device are respectively arranged on the test bench; the upper rotor testing device comprises an upper rotor driving part, a first force sensor and a first torque sensor, the upper rotor driving part is used for driving an upper testing rotor to rotate, the first force sensor is used for testing the tensile force borne by the upper testing rotor, and the first torque sensor is used for testing the torque borne by the upper testing rotor during rotation; the lower rotor testing device comprises a lower rotor driving part, a second force sensor and a second torque sensor, the lower rotor driving part is used for driving the lower testing rotor to rotate, the second force sensor is used for testing the tensile force borne by the lower testing rotor, and the second torque sensor is used for testing the torque borne by the lower testing rotor during rotation. According to the scheme provided by the invention, the double rotors which are arranged up and down can be tested at the same time.

    本申请涉及一种飞行器旋翼测试设备。该飞行器旋翼测试设备包括:测试台架及分别设于所述测试台架上的上旋翼测试装置和下旋翼测试装置;所述上旋翼测试装置包括上旋翼驱动件、第一力传感器和第一扭矩传感器,所述上旋翼驱动件用于驱动上测试旋翼旋转,所述第一力传感器用于测试上测试旋翼所受的拉力,所述第一扭矩传感器用于测试上测试旋翼旋转时所受的扭矩;所述下旋翼测试装置包括下旋翼驱动件、第二力传感器和第二扭矩传感器,所述下旋翼驱动件用于驱动下测试旋翼旋转,所述第二力传感器用于测试下测试旋翼所受的拉力,所述第二扭矩传感器用于测试下测试旋翼旋转时所受的扭矩。本申请提供的方案,能够同时对上下布置的双旋翼进行测试。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft rotor test equipment


    Weitere Titelangaben:

    飞行器旋翼测试设备


    Beteiligte:
    LIU JINLONG (Autor:in) / WU JIEBO (Autor:in) / JIANG KANG (Autor:in) / HE HONGJIAN (Autor:in) / XU WENLONG (Autor:in) / GU WEIJIAN (Autor:in) / LU XIONGJIAN (Autor:in) / HUANG JINTENG (Autor:in) / CHEN SHUO (Autor:in) / ZHOU ZHOU (Autor:in)

    Erscheinungsdatum :

    2023-07-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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



    Rotor aircraft test platform

    ZHANG XINYU / LIU YAO | Europäisches Patentamt | 2015

    Freier Zugriff

    Tilt-rotor aircraft rotor system test bench and test method

    HE YUQING / GU FENG / YU LI et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Rotor aircraft near-surface effect test device

    BAI XINGZHI / YU DAICHUAN / XING BEIBEI et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Rotor wing driving equipment and aircraft

    ZHANG ZHIQIANG / GU WANPENG | Europäisches Patentamt | 2023

    Freier Zugriff

    Balance test system of four-rotor aircraft

    JING BENQIN / GE RENHUA / LIU GANGLING et al. | Europäisches Patentamt | 2015

    Freier Zugriff