| 发明名称 |
WING AERIAL REFUELING SYSTEM |
| 摘要 |
An aircraft comprises a wing assembly, a pod, and a pylon attaching the pod to the wing assembly. The pylon has a swept pylon flap, 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 |
US2016144950(A1) |
申请公布日期 |
2016.05.26 |
| 申请号 |
US201414256935 |
申请日期 |
2014.04.19 |
| 申请人 |
The Boeing Company |
发明人 |
Ferguson Stanley D.;Fialho Ian J.;Potter Richard C. |
| 分类号 |
B64C23/00;B64D39/00 |
主分类号 |
B64C23/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft comprising:
a wing assembly; a pod; and a pylon attaching the pod to the wing assembly, the pylon having a swept pylon flap, the swept pylon flap 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. |
| 地址 |
Chicago IL US |
