The invention relates to the technical field of aircrafts, in particular to an aircraft electrical control system which comprises a system body, a control panel and a warning lamp and further comprises a protection assembly, the protection assembly comprises a moving block, a connecting frame, a mounting frame and a moving component, the moving block is connected with the system body through the moving component, and the connecting frame is fixedly connected with the moving block. The mounting frame is fixedly connected with the connecting frame and the warning lamp, the moving component is arranged on the system body and connected with the moving block, and the warning lamp can move into the system body, so that the warning lamp is protected through a protective shell of the system body; and damage caused by collision outside the system body when the warning lamp is not used is avoided.

    本发明涉及航空器技术领域,具体涉及一种飞机电气控制系统,包括系统本体、控制面板和警示灯,还包括防护组件,防护组件包括移动块、连接架、安装架和移动构件,移动块与系统本体通过移动构件连接,连接架与移动块固定连接,安装架分别与连接架和警示灯固定连接,移动构件设置在系统本体上,并与移动块连接,通过将警示灯能够移动进入到系统本体中,从而通过系统本体的保护外壳来实现对警示灯的保护,避免警示灯未使用时在系统本体外受到磕碰而造成损坏。


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    Titel :

    Aircraft electrical control system


    Weitere Titelangaben:

    一种飞机电气控制系统


    Beteiligte:
    LIU XIJUN (Autor:in)

    Erscheinungsdatum :

    04.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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