| 发明名称 |
WING AERIAL REFUELING SYSTEM |
| 摘要 |
An aircraft (110) comprises a wing assembly (130), a pod (176), and a pylon (178) attaching the pod (176) to the wing assembly (130). The pylon (178) has a swept pylon flap (410), which is configured to unload the pylon and pod during flight of the aircraft, and also to create downward flow that counters a vortex trailing the pod. |
| 申请公布号 |
EP2933185(A1) |
申请公布日期 |
2015.10.21 |
| 申请号 |
EP20150163131 |
申请日期 |
2015.04.10 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
FERGUSON, STANLEY D;FIALHO, IAN J;POTTER, RICHARD C |
| 分类号 |
B64C23/00;B64D29/02;B64D39/00 |
主分类号 |
B64C23/00 |
| 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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