The invention discloses an airtight cabin penetrating device and method in an aircraft towing cable cabin. Comprising an installation hole (5) formed in an airtight cabin wall (4), a cabin penetrating sleeve (1) is installed in the installation hole (5) in a sealed mode, guide limiting assemblies (3) are arranged at the two ends of an inner cylinder of the cabin penetrating sleeve (1), and a gap control assembly (2) is arranged between the two guide limiting assemblies (3). The problem that a long-size dragging cable penetrates through an airtight line at a high speed in a cabin is solved, and it is guaranteed that the cable is smoothly wound and unwound within a large size range.

    本发明公开了一种飞机拖曳缆索舱内气密穿舱装置及方法。包括设置于气密舱壁(4)上的安装孔(5),安装孔(5)内密封安装有穿舱套筒(1),穿舱套筒(1)内筒的两端均设有导向限位组件(3),两导向限位组件(3)间设有间隙控制组件(2)。本发明解决了长尺寸拖曳缆索在舱内高速穿越气密线的问题,保障缆索在较大尺寸范围内顺畅收放。


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    Titel :

    Airtight cabin penetrating device and method in aircraft towing cable cabin


    Weitere Titelangaben:

    一种飞机拖曳缆索舱内气密穿舱装置及方法


    Beteiligte:
    GUAN DONGJIE (Autor:in) / CHEN YANQIANG (Autor:in) / LI ZHEN (Autor:in) / LIANG HU (Autor:in) / SUN KE (Autor:in) / HUANG CAIFU (Autor:in) / LI WENKE (Autor:in) / HAN DONGJIANG (Autor:in) / QIAO LEI (Autor:in) / WANG JIANQIANG (Autor:in)

    Erscheinungsdatum :

    2024-04-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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