发明名称 |
AIRCRAFT WING WITH WING TIP DEVICE |
摘要 |
An aircraft wing assembly including: a wing having a wing box structure with an upper wing cover and a lower wing cover, and a wing tip device attached to the outboard end of the wing, the wing tip device including an upper cover and a lower cover, wherein a gap between opposing edges of the wing tip device lower cover and the lower wing cover is at least 5 mm, a seal assembly aerodynamically seals the gap, wherein the seal assembly includes a bridging component on an interior side of the gap, and a seal which fills the gap and is supported by the bridging component. |
申请公布号 |
US2017008616(A1) |
申请公布日期 |
2017.01.12 |
申请号 |
US201615273239 |
申请日期 |
2016.09.22 |
申请人 |
Airbus Operations Limited |
发明人 |
DAVIES Huw;McKENNA Nigel |
分类号 |
B64C23/06;B64C3/00 |
主分类号 |
B64C23/06 |
代理机构 |
|
代理人 |
|
主权项 |
1. An aircraft wing assembly comprising:
a wing having a wing box structure including an upper wing cover and a lower wing cover; a wing tip device attached to an outboard end of the wing, the wing tip device including an upper cover and a lower cover, wherein a gap between opposing edges of the wing tip device lower cover and the lower wing cover is at least 5 mm; and a seal assembly configured to aerodynamically seal the gap, wherein the seal assembly includes a bridging portion extending across an interior side of the gap to bridge the gap, and a seal portion which projects from the bridging portion to fill the gap. |
地址 |
Bristol GB |