A resilient and elongate tubular seal that is flexible and has a cross-section of a selected geometry and that is capable of absorbing compressive forces to seal a gap between adjacently positioned aircraft cabin structures, and a method of installing such a tubular seal are disclosed. And the tubular sealing element can expand outwards when the compression force is changed or reduced.
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。
Aircraft cabin seal
飞机机舱密封件
2024-07-26
Patent
Electronic Resource
Chinese