The invention discloses a helicopter tail rotor simulation system for a wind tunnel test. The system comprises a base, a driving mechanism, a supporting arm, a tilting adjustment mechanism and a tailrotor transmission measurement control module, wherein one end of the supporting arm is a fixed end, the other end is a tilting end, the fixed end of the supporting arm is rotatably connected with thebase, the driving mechanism is used for driving the supporting arm to rotate around the base, the tilting adjusting mechanism is installed at the tilting end of the supporting arm and can move in theaxial direction of the supporting arm and rotate around the axial direction of the supporting arm, and the tail rotor transmission measurement control module is rotatably connected with the tilting adjustment mechanism. Flight states of different helicopters at different inclination angles can be simulated.

    本发明公开了一种风洞试验用直升机尾桨模拟系统,其包括基座、驱动机构、支撑臂、倾转调节机构和尾桨传动测量操纵模块,支撑臂的一端为固定端,另一端为倾转端,支撑臂的固定端与基座转动连接,驱动机构用于驱动支撑臂绕基座转动,倾转调节机构安装在支撑臂的倾转端,倾转调节机构能够沿支撑臂的轴向移动以及绕支撑臂的轴向转动,尾桨传动测量操纵模块与倾转调节机构转动连接。本发明能够模拟不同直升机在不同倾角下的飞行状态。


    Access

    Download


    Export, share and cite



    Title :

    Helicopter tail rotor simulation system for wind tunnel test


    Additional title:

    一种风洞试验用直升机尾桨模拟系统


    Contributors:
    HUANG ZHIYUAN (author) / YANG YONGDONG (author) / PENG XIANMIN (author) / ZHANG GUICHUAN (author) / TANG MIN (author) / ZHAO LIANGLIANG (author)

    Publication date :

    2020-08-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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



    Helicopter rotor model icing wind tunnel test method

    YUAN HONGGANG / HUANG MINGQI / PENG XIANMIN et al. | European Patent Office | 2020

    Free access


    Helicopter rotor tail rotor failure protection system and helicopter

    CHEN XI / GAO XUAN / FEI ZHONGYANG et al. | European Patent Office | 2023

    Free access

    Helicopter tail rotor noise

    CHOU, S.-T. / GEORGE, A. | AIAA | 1986


    Helicopter without tail rotor

    PENG ZUOJUN / PENG HAO | European Patent Office | 2020

    Free access