The invention relates to aircraft canopy opening and closing control equipment and a control method, and belongs to the technical field of aircraft electromechanical control. An aircraft canopy opening and closing control device comprises a front cabin cover opening and closing switch and a rear cabin cover opening and closing switch which are arranged on a front cabin and a rear cabin of an aircraft respectively, and the cabin cover opening and closing switches can achieve state switching of the cabin opening position, the cabin closing position and the neutral position. The cabin cover opening and closing button box is arranged outside the cabin and comprises a cabin opening button and a cabin closing button; when the canopy is in an opened or closed state, the canopy is controlled to be opened and closed through the canopy opening and closing button box. The system has the following advantages that canopy opening and closing control is integrated into electromechanical load power distribution equipment, the number of airborne finished products is reduced, the weight of the finished products is reduced, the execution efficiency of an electric mechanism is improved, relevant parameters can be stored and recorded in real time, and later maintenance of a canopy system is facilitated.

    本发明涉及一种飞机座舱盖启闭控制设备及控制方法,属于飞机机电控制技术领域。一种飞机座舱盖启闭控制设备,包括分别设置在飞机前座舱、后座舱的前舱舱盖启闭开关、后舱舱盖启闭开关,舱盖启闭开关可实现开舱、关舱和中立三个位置的状态切换;还包括设置在座舱外部的舱盖启闭按钮盒,其包括开舱和关舱按钮;当座舱盖处于开启或者关闭状态时,通过舱盖启闭按钮盒实现对座舱盖开启与关闭的控制。本发明具有如下优点:实现了将座舱盖启闭控制集成到机电负载配电设备中,减少了机载成品数量和降低了成品重量,提高了电动机构的执行效率,相关参数均可实时存储记录,便于后期座舱盖系统的维护。


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    Titel :

    Aircraft canopy opening and closing control equipment and control method


    Weitere Titelangaben:

    一种飞机座舱盖启闭控制设备及控制方法


    Beteiligte:
    FU YING (Autor:in) / LI ZHILONG (Autor:in) / ZHOU BING (Autor:in) / SHANG HUI (Autor:in) / ZHANG LISHENG (Autor:in) / LIU LONG (Autor:in) / DAI HUIZHEN (Autor:in) / WU JIANJING (Autor:in) / JIANG ZUXIN (Autor:in) / CAO CHAOHUA (Autor:in)

    Erscheinungsdatum :

    2022-10-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64C AEROPLANES , Flugzeuge



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