| 发明名称 |
Variable geometry nacelle for an aircraft engine and corresponding operating method |
| 摘要 |
A nacelle assembly (26) includes an inlet lip section (38) and a cowl section (50) positioned downstream of the inlet lip section (38). At least a portion (52) of the cowl section (50) is moveable to influence an effective boundary layer thickness of the nacelle assembly (26). |
| 申请公布号 |
EP1992807(B1) |
申请公布日期 |
2016.09.07 |
| 申请号 |
EP20080251734 |
申请日期 |
2008.05.16 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
JAIN, ASHOK K. |
| 分类号 |
F02C7/042;F02K1/42;F02K3/06;F02K3/077 |
主分类号 |
F02C7/042 |
| 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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