| 发明名称 |
THERMALLY CONFORMABLE LINER FOR REDUCING SYSTEM LEVEL FAN BLADE OUT LOADS |
| 摘要 |
<p>A fan case for a gas turbine engine includes a fan case surrounding a fan with fan blades. A liner is disposed between the fan case and the fan and is spaced a radial distance from the fan case. A torque stop is arranged between the fan case and the liner. A method for reducing fan case liner loads is also disclosed.</p> |
| 申请公布号 |
WO2014197031(A2) |
申请公布日期 |
2014.12.11 |
| 申请号 |
WO2014US22932 |
申请日期 |
2014.03.11 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HUSBAND, JASON;LANCASTER, DREW, W. |
| 分类号 |
F02C7/24;F01D25/08;F04D29/58 |
主分类号 |
F02C7/24 |
| 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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