A system and method for a wing emergency exit door is provided. The wing emergency exit door system includes a door, a handle connected to an inside surface of the door, a guide rail connected to a body of the aircraft, a roller, a first crank connected to the roller and associated with the handle, a first shaft system attached to the first crank, a latch system connected to the first shaft system, and a locking system associated with the latch system. The latch system includes a rotation stop, a second crank associated with the rotation stop, and a second shaft system connected to the second crank and the rotation stop. The components together control operation of the wing emergency exit door between an open position and a closed position.

    提供了一种用于机翼紧急出口门的系统和方法。该机翼紧急出口门系统包括门、连接至门的内侧表面的手柄、连接至飞机的主体的导轨、滚轮、连接至滚轮并与手柄相关联的第一曲柄、附接到第一曲柄的第一轴系统、连接至第一轴系统的闩锁系统、以及与闩锁系统相关联的锁定系统。闩锁系统包括旋转止挡件、与旋转止挡件相关联的第二曲柄以及连接至第二曲柄和旋转止挡件的第二轴系统。这些部件一起控制机翼紧急出口门在打开位置和关闭位置之间的操作。


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    Titel :

    Wing emergency exit door system


    Weitere Titelangaben:

    机翼紧急出口门系统


    Beteiligte:

    Erscheinungsdatum :

    01.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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