The invention belongs to the technical field of helicopter flight control systems, and discloses a helicopter flight control system comprehensive display method. The helicopter flight control system is improved on the basis of an original flight control system, the working state display mode of the flight control system is comprehensively changed, control surface position indicator equipment is canceled, and control surface position indication, modal input, prompt and other information are comprehensively displayed on a multifunctional display. According to the flight control system comprehensive display design method, display information related to the flight control system is achieved on the multifunctional displayer, and a driver can check the state of the flight control system easily and pay attention to flight on the whole body.

    本发明属于直升机飞行控制系统技术领域,公开了一种直升机飞控系统综合显示方法。直升机飞控系统在原有飞控系统基础上改进,对飞控系统工作状态显示方式进行了全面的改变,取消了舵面位置指示器设备,将舵面位置指示、模态投入、提示等信息综合显示在多功能显示器上,通过该飞控系统综合显示设计方法,与飞控系统有关的显示信息均在多功能显示器上实现,驾驶员可以较轻松查看飞控系统状态,将精力全身关注在飞行上。


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    Title :

    Helicopter flight control system comprehensive display method


    Additional title:

    一种直升机飞控系统综合显示方法


    Contributors:
    ZHANG HAOHUA (author) / ZHAO DANLI (author) / CHENG DONGQUAN (author)

    Publication date :

    2021-02-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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