发明名称 Seal assembly for an aircraft wing
摘要 <p>A wing assembly 2 for an aircraft 1 comprising a spar 3, a wing cover 4 and a rib 5; wherein the spar has a web portion 3a and a flange portion 3b joined by a radius corner 3c; wherein a gap 6 is formed at an interface between the spar, the wing cover and the rib; wherein the assembly further comprises a seal member 7 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.</p>
申请公布号 EP2641830(A3) 申请公布日期 2015.06.03
申请号 EP20130157422 申请日期 2013.03.01
申请人 AIRBUS OPERATIONS LIMITED 发明人 WILSON, JAMES;QUAYLE, ALAN;HADLEY, PAUL
分类号 B64C3/18;B64C3/26;B64C3/28 主分类号 B64C3/18
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