| 发明名称 |
AIRCRAFT WITH A WING TIP COMPRISING A FUEL POD |
| 摘要 |
An aircraft comprising a wing, the wing having a connection interface at the tip of the wing, and the wing being interchangeable between a first configuration in which a first wing tip is connected to the connection interface, and a second configuration in which a second wing tip is connected to the connection interface to replace the first wing tip. The second wing tip comprises a fuel pod for carrying additional fuel, and a wing tip device for improving aerodynamic efficiency. The wing may be designed for performance in both configurations. |
| 申请公布号 |
US2016130012(A1) |
申请公布日期 |
2016.05.12 |
| 申请号 |
US201514933321 |
申请日期 |
2015.11.05 |
| 申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
LAGUIA-BARNOLA Roger;ORCHARD Matthew Noel;WOOD Norman |
| 分类号 |
B64D37/04;G06Q10/06;G06Q30/06;B64C3/38;B64C23/06 |
主分类号 |
B64D37/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft comprising an aircraft wing, the wing having a connection interface at the tip of the wing, and the wing being interchangeable between a first configuration in which a first wing tip is connected to the connection interface, and a second configuration in which a second wing tip is connected to the connection interface to replace the first wing tip,
wherein the second wing tip comprises a fuel pod and wherein the wing has been designed for performance in both the first and the second configurations. |
| 地址 |
Bristol GB |
