| 发明名称 |
Engine pylon for the suspension of a turbo engine under an aircraft wing |
| 摘要 |
According to the invention, the engine pylon for the suspension of a turbo engine under an aircraft wing is such that the trailing edge of the rear lower part of the engine pylon is shifted toward the root of the wing. |
| 申请公布号 |
US8336813(B2) |
申请公布日期 |
2012.12.25 |
| 申请号 |
US20090550454 |
申请日期 |
2009.08.31 |
| 申请人 |
BONNAUD CYRIL;FOL THIERRY;DUMOULIN ANNE;GIBSON TOM;LYONS NEIL;AIRBUS OPERATIONS SAS;AIRBUS UK LIMITED |
发明人 |
BONNAUD CYRIL;FOL THIERRY;DUMOULIN ANNE;GIBSON TOM;LYONS NEIL |
| 分类号 |
B64D27/00 |
主分类号 |
B64D27/00 |
| 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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