The invention provides a debugging method and debugging equipment for a helicopter integrated pedal control device, and relates to the technical field of helicopter cockpit control systems. According to the method, control angle testing assemblies are installed on a pedal stand column and the tiptoe of a pedal respectively, and a control force testing assembly is installed at the force application point of the pedal. The pedal stand column is provided with a control angle testing device to display the tilting angle of the stand column, and the tilting angle of the stand column represents the tilting angle and the control displacement of the pedal. A control force testing device is arranged at a force application point (the geometric center of a pedal rotating shaft) of the pedal and is used for measuring control force; and a control angle testing device is arranged at the tiptoe of the pedal to test the brake control stroke of the pedal. According to the method, the dynamic characteristics of the helicopter integrated pedal control device and the nonlinear characteristics in the movement process can be visually and accurately tested, and a basis is provided for design, optimization and improvement of the helicopter integrated pedal control device.

    本申请提供了一种直升机集成化脚蹬操纵装置的调试方法及调试设备,涉及直升机驾驶舱操纵系统技术领域。该方法在脚蹬立柱上以及脚蹬踏板脚尖处的分别安装操纵角度测试组件、在脚蹬踏板施力点处安装操纵力测试组件。脚蹬立柱上配备操纵角度测试装置来显示立柱的倾转角度,而立柱的倾转角度代表脚蹬踏板的倾转角度和操纵位移;在脚蹬踏板施力点处(踏板转轴几何中心)设置操纵力测试装置,用来测量操纵力;在脚蹬踏板脚尖处设置操纵角度测试装置来测试脚蹬踏板刹车操纵行程。该方法可以直观准确地测试出直升机集成化脚蹬操纵装置的动态特性及运动过程中的非线性特性,为直升机集成化脚蹬操纵装置的设计和优化改进提供依据。


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    Titel :

    Debugging method and debugging equipment for integrated pedal operating device of helicopter


    Weitere Titelangaben:

    一种直升机集成化脚蹬操纵装置的调试方法及调试设备


    Beteiligte:
    WANG WEN (Autor:in) / WEI YULONG (Autor:in) / QI WEIMING (Autor:in) / YANG ZIHAO (Autor:in) / DING YUNPENG (Autor:in)

    Erscheinungsdatum :

    11.04.2025


    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



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