| 发明名称 |
Wing tip device with recess in surface |
| 摘要 |
An aerodynamic lift structure includes a wing and at least one wing tip device at an outboard portion of the wing. A surface of each wing tip device has a recess that reduces flow impact at a junction of the wing and the wing tip device. |
| 申请公布号 |
US8651427(B1) |
申请公布日期 |
2014.02.18 |
| 申请号 |
US201213411941 |
申请日期 |
2012.03.05 |
| 申请人 |
MALACHOWSKI ADAM P.;CHANEY STEPHEN R.;EBNER NORMAN K.;LEDOUX STEPHEN L.;VEGTER CHRISTOPHER A.;THE BOEING COMPANY |
发明人 |
MALACHOWSKI ADAM P.;CHANEY STEPHEN R.;EBNER NORMAN K.;LEDOUX STEPHEN L.;VEGTER CHRISTOPHER A. |
| 分类号 |
B64C3/58;B64C23/06 |
主分类号 |
B64C3/58 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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