|국가/구분||United States(US) Patent 등록|
|§371/§102 date||20131220 (20131220)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 4|
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 bridgi...
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 the outboard end of the wing, wherein the wing tip device includes an upper cover and a lower cover;a gap of at least 5 mm between opposing edges of the lower cover of the wing tip device and the lower wing cover;a seal assembly configured to aerodynamically seal the gap, wherein the seal assembly includes a bridging component on an interior side of the gap and a seal, wherein the seal fills the g...