| 发明名称 |
Guide vane for a gas turbine engine |
| 摘要 |
A guide vane for a gas turbine aircraft engine includes an aerodynamic shell for turning a flow of working fluid and an internal spar spaced from the aerodynamic shell by an air gap and reinforced by stiffeners.
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| 申请公布号 |
US2008056888(A1) |
申请公布日期 |
2008.03.06 |
| 申请号 |
US20060515101 |
申请日期 |
2006.09.01 |
| 申请人 |
UNITED TECHNOLOGIES |
发明人 |
SOMANATH NAGENDRA;KUMAR KESHAVA B. |
| 分类号 |
F01D25/16 |
主分类号 |
F01D25/16 |
| 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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