发明名称 Aircraft wing with wing tip device
摘要 An aircraft wing assembly comprising a wing (2) having a wing box structure including an upper wing cover (7) and a lower wing cover (8), and a wing tip device (1) attached to the outboard end of the wing, the wing tip device including an upper cover (9) and a lower cover (10), wherein a gap (g) between opposing edges of the wing tip device lower cover (10) and the lower wing cover (8) is at least 5 mm, and further comprising a seal assembly (20) for aerodynamically sealing the gap (g), wherein the seal assembly (20) includes a bridging component (21) on an interior side of the gap (g), and a seal (22) which fills the gap (g) and is supported by the bridging component (21). Also, an aircraft having the wing assembly, and a method of attaching a wing tip device (1) to the outboard end of a wing (2).
申请公布号 GB201110493(D0) 申请公布日期 2011.08.03
申请号 GB20110010493 申请日期 2011.06.21
申请人 AIRBUS OPERATIONS LTD 发明人
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