The invention relates to an auxiliary barrier for an aircraft. An example auxiliary barrier includes a plurality of rails mounted to a first construction in a cabin of an aircraft and a plurality of rods, with respective ones of the rods slidably engaging respective ones of the rails. The auxiliary barrier includes panels coupled to respective ends of the rods. The rod moves relative to the track between a stowed position and a deployed position. The panel in the deployed position mates with a second construction in the nacelle opposite the first construction. The rod extends between the first construction and the second construction when the auxiliary barrier is in the deployed position.

    本发明涉及用于飞机的辅助屏障。示例性辅助屏障包括多个轨道和多个杆,所述多个轨道安装到飞机的机舱中的第一建构物,其中,所述杆中的相应杆能滑动地接合所述轨道中的相应轨道。所述辅助屏障包括联接到所述杆的相应端部的面板。所述杆相对于所述轨道在收起位置与展开位置之间移动。处于所述展开位置的所述面板与所述机舱中的与所述第一建构物相对的第二建构物配合。当所述辅助屏障处于所述展开位置时,所述杆在所述第一建构物和所述第二建构物之间延伸。


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    Title :

    Auxiliary barrier for aircraft


    Additional title:

    用于飞机的辅助屏障



    Publication date :

    2023-11-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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