| 发明名称 |
CORRUGATED CORE COWL FOR A GAS TURBINE ENGINE |
| 摘要 |
<p>An example core nacelle for a gas turbine engine includes a core cowl positioned adjacent to an inner duct boundary of a fan bypass passage having an associated cross-sectional area. The core cowl includes at least one groove that is selectively exposed to change the cross-sectional area.</p> |
| 申请公布号 |
WO2008045035(A1) |
申请公布日期 |
2008.04.17 |
| 申请号 |
WO2006US39050 |
申请日期 |
2006.10.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION;BALTAS, CONSTANTINE |
发明人 |
BALTAS, CONSTANTINE |
| 分类号 |
F02K1/06 |
主分类号 |
F02K1/06 |
| 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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