The invention discloses a civil aviation passenger plane reverse thrust hydraulic power system test platform, and particularly relates to the technical field of power testing, the civil aviation passenger plane reverse thrust hydraulic power system test platform comprises a test module, the test module is connected with an adjusting unit, the test module is connected with a frequency adjusting unit and a counting module, and the frequency adjusting unit and the counting module are both connected with a central controller. The temperature, the humidity and the pressure of the environment where the test module is located are adjusted, the working conditions of the reverse thrust hydraulic power system under different external conditions are simulated, the change of operation data of the reverse thrust hydraulic power system when the reverse thrust hydraulic power system operates for different times is tested and recorded, and according to various test data, the test module can be used for testing the reverse thrust hydraulic power system. The power data output by the reverse thrust hydraulic power system in the actual working environment is judged, the actually output power data is compared with the required power data, and the power compensation operation is performed, so that the requirement of the reverse thrust process is accurately met, and the whole test process is more flexible and fits the actual working environment.

    本发明公开了一种民航客机反推液压动力系统测试平台,具体涉及动力测试技术领域,包括测试模块,所述测试模块与调整单元连接,所述测试模块与频率调节单元和计数模块连接,所述频率调节单元和计数模块均与中央控制器连接。本发明通过对测试模块所处环境中的温度、湿度和压力进行调整,模拟反推液压动力系统在不同外部条件下的工作情况,对反推液压动力系统运行不同次数时其运行数据的变化进行测试记录,根据各种测试数据,判断反推液压动力系统在实际的工作环境中所输出的动力数据,根据实际输出的动力数据与所需的动力数据进行比对,进行动力的补偿操作,使其精准达到反推过程的需求,使整体的测试过程更为灵活,且贴合实际工作环境。


    Access

    Download


    Export, share and cite



    Title :

    Civil aircraft backstepping hydraulic power system test platform


    Additional title:

    一种民航客机反推液压动力系统测试平台


    Contributors:
    DAI HUI (author) / YANG MENG (author)

    Publication date :

    2023-08-29


    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 / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G06M COUNTING MECHANISMS , Zählwerke / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen



    Gust load alleviation control of civil aircraft based on backstepping

    Bai, Xuefei / Zhang, Shaojie / Li, Zhengqiang | IEEE | 2014


    Civil aircraft hydraulic system pipeline integration testing device

    DENG YUDONG / ZHANG YINGWEI / LI SHIHE | European Patent Office | 2024

    Free access


    Comprehensive maintenance platform for civil aircraft

    ZHAO BO / XU TAO / TANG KE | European Patent Office | 2025

    Free access

    Variable-configuration experimental platform for civil aircraft emergency evacuation simulation test

    PENG HAOXUAN / LIU XIAOCHUAN / HUI XULONG et al. | European Patent Office | 2024

    Free access