| 发明名称 |
WING TIP DEVICE FOR AN AIRCRAFT WING |
| 摘要 |
A wing tip device for an aircraft wing may include an upper winglet and a lower element. The upper winglet may extend upwardly from an aircraft wing. The lower element may extend downwardly from the upper winglet and may form a closed loop below the wing. The closed loop may have a hollow interior. |
| 申请公布号 |
US2016144951(A1) |
申请公布日期 |
2016.05.26 |
| 申请号 |
US201414251601 |
申请日期 |
2014.04.12 |
| 申请人 |
The Boeing Company |
发明人 |
Zaman AbuMuhammed A. |
| 分类号 |
B64C23/06;B64F5/00 |
主分类号 |
B64C23/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A wing tip device for an aircraft wing, comprising:
an upper winglet configured to extend upwardly from an aircraft wing; and a lower element extending downwardly from the upper winglet and configured to form a closed loop below the wing, the closed loop having a hollow interior. |
| 地址 |
Chicago IL US |
