| 发明名称 |
AIRCRAFT WING WITH A WING TIP DEVICE AND A STRUT |
| 摘要 |
An aircraft wing (1) has a wing tip device (3) joined thereto. The root (7) of the wing tip device (3) is joined to the tip of the wing (1) at a first connection (11). An external strut (9) extends between the wing (1) and the wing tip device (3), the strut (9) being joined to the wing (1) at a second connection (13). The second connection (13) is inboard of the first connection, such that loadings on the wing tip device (3) generated during use, are transferred, via the strut (9), to a location on the wing (1) that is inboard of where the root (7) of the wing tip device (3) is joined to the tip of the wing. |
| 申请公布号 |
US2017029094(A1) |
申请公布日期 |
2017.02.02 |
| 申请号 |
US201515301489 |
申请日期 |
2015.04.02 |
| 申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
LYNAS Christopher;THOMPSON Robert;WILLIAMS Llifon;HOBDAY John |
| 分类号 |
B64C23/06;B64C3/54 |
主分类号 |
B64C23/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft wing having a wing tip device joined thereto,
wherein the root of the wing tip device is joined to the tip of the wing at a first connection, and wherein an external strut extends between the wing and the wing tip device, the strut being joined to the wing at a second connection, the second connection being inboard of the first connection, such that loadings on the wing tip device generated during use, are transferred, via the strut, to a location on the wing that is inboard of where the root of the wing tip device is joined to the tip of the wing. |
| 地址 |
Bristol GB |
