| 发明名称 |
Variable geometry nacelle with nanoelectromechanical system for an aircraft engine and corresponding operating method |
| 摘要 |
<p>A nacelle assembly (26) includes an inlet lip section (38) and a cowl section (50) downstream of the inlet lip section (38). At least a portion of the cowl section (50) is flexed to take various shapes through a nanoelectromechanical system (64) and thereby influence an effective boundary layer thickness of the nacelle assembly (26).</p> |
| 申请公布号 |
EP2003309(A2) |
申请公布日期 |
2008.12.17 |
| 申请号 |
EP20080252040 |
申请日期 |
2008.06.13 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
JAIN, ASHOK K. |
| 分类号 |
F02C7/042;F02C7/045;F02K3/06 |
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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