| 发明名称 |
Nacelle-To-Pylon Fairing |
| 摘要 |
A nacelle-to-pylon fairing formed over at least a portion of an inter-region between a nacelle and a pylon of an aircraft may include a longitudinal axis, a lateral axis and a transverse axis, an upper end incorporated to the pylon at a fairing-to-pylon interface, and a lower end incorporated to the nacelle at a fairing-to-nacelle interface, wherein the fairing defines a surface between the upper end and the lower end. |
| 申请公布号 |
US2015321766(A1) |
申请公布日期 |
2015.11.12 |
| 申请号 |
US201414270485 |
申请日期 |
2014.05.06 |
| 申请人 |
The Boeing Company |
发明人 |
Howe Sean P.;Gromek Christopher L.;Taylor Anish A. |
| 分类号 |
B64D29/06;B64D29/02;B64D27/26;B64C7/02 |
主分类号 |
B64D29/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fairing formed over at least a portion of an inter-region between a nacelle and a pylon of an aircraft, said fairing comprises:
a longitudinal axis, a lateral axis and a transverse axis; an upper end incorporated with said pylon at a fairing-to-pylon interface; and a lower end incorporated with said nacelle at a fairing-to-nacelle interface, wherein said fairing defines a surface between said upper end and said lower end. |
| 地址 |
Chicago IL US |
