公开了一种弹性且细长的管状密封件以及一种安装这种管状密封件的方法,该管状密封件是柔性的并且具有选定几何形状的截面,并且该管状密封件能够吸收压缩力以密封相邻定位的飞机机舱结构之间的间隙,并且该管状密封件还能够在压缩力变化或减小时向外膨胀。

    Resilient elongated tubular seals that are flexible and that comprise selected geometric cross-sections and that can absorb compressive forces to seal gaps between adjacently positioned aircraft cabin structure and that can further expand outwardly as compressive forces change or abate and methods of installation of such tubular seals are disclosed.


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    Titel :

    飞机机舱密封件


    Erscheinungsdatum :

    2024-07-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F16J Kolben , PISTONS / B64C AEROPLANES , Flugzeuge