| 发明名称 |
AIRPLANE HAVING ENGINES PARTIALLY ENCASED IN THE FUSELAGE |
| 摘要 |
<p>An airplane provided with dual-flow turbojet engines having nacelles at least partially encased in the fuselage, wherein the air intake of each engine is connected to the fuselage by two boundary layer guiding walls, the walls extending towards the upstream side of the air intake and being spaced apart towards the upstream side.</p> |
| 申请公布号 |
EP2340203(B1) |
申请公布日期 |
2012.12.05 |
| 申请号 |
EP20090755936 |
申请日期 |
2009.10.28 |
| 申请人 |
SNECMA |
发明人 |
CHANEZ, PHILIPPE, GERARD;LECORDIX, JEAN-LOIC, HERVE;THOMAS, STEPHANE, JACQUES, FRANCOIS |
| 分类号 |
B64D29/04;B64C1/00;B64C7/02 |
主分类号 |
B64D29/04 |
| 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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