| 发明名称 |
AIRCRAFT WING FOR RECEIVING A PLURALITY OF DIFFERENT WING TIP DEVICES |
| 摘要 |
An aircraft wing, the wing having a connection interface at the tip of the wing, and the wing being configurable between a first configuration in which a first wing tip device is connected to the connection interface, and a second configuration in which a second wing tip device is connected to the connection interface to replace the first wing tip device. The design of the wing is such that it is designed for performance in both the first and the second configurations. |
| 申请公布号 |
US2016129993(A1) |
申请公布日期 |
2016.05.12 |
| 申请号 |
US201514933126 |
申请日期 |
2015.11.05 |
| 申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
DEE Jonathan;ORCHARD Matthew Noel |
| 分类号 |
B64C23/06;G06Q30/06;G06F17/50;B64C3/38 |
主分类号 |
B64C23/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of designing a wing for an aircraft, the wing having a connection interface at its tip for receiving a plurality of different wing tip devices, and the wing being configurable between a first configuration in which a first wing tip device is connected to the connection interface, and a second configuration in which the first wing tip device is replaced by a second wing tip device connected to the connection interface,
wherein the method comprises the step of
designing the wing for performance in both the first configuration and the second configuration. |
| 地址 |
Bristol GB |
