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发明公开
CN103318402A 用于飞机翼的密封组件 失效 - 放弃专利权

用于飞机翼的密封组件
摘要：
本发明公开了一种用于飞机的翼组件，该翼组件包括翼梁、翼盖和肋；其中翼梁具有通过半径角部连接的腹板部分和凸缘部分；其中间隙形成在翼梁、翼盖和肋之间的界面处；其中该组件还包括：基本上覆盖该间隙的密封构件，和布置在密封构件与肋和/或翼盖和/或翼梁之间以便密封该间隙的密封剂。而且，本发明还公开了一种用来密封飞机翼组件中的间隙的方法。
摘要（英）：

A wing assembly for an aircraft comprising a spar, a wing cover and a rib; wherein the spar has a web portion and a flange portion joined by a radius corner; wherein a gap is formed at an interface between the spar, the wing cover and the rib; wherein the assembly further comprises a seal member which substantially covers the gap, and sealant provided between the seal member and the rib and/or the wing cover and/or the spar so as to seal the gap. Also a method for sealing a gap in an aircraft wing assembly.

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