| 发明名称 |
Airfoil locator rib and method of positioning an insert in an airfoil |
| 摘要 |
An airfoil for a gas turbine engine, the airfoil comprising a locator rib provided at a bottom of a cavity in the airfoil core, the locator rib having an inclined surface to be engaged by a leading end of the insert during installation thereof in the cavity.
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| 申请公布号 |
US2006177309(A1) |
申请公布日期 |
2006.08.10 |
| 申请号 |
US20050049977 |
申请日期 |
2005.02.04 |
| 申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
SYNNOTT REMY;DUROCHER ERIC |
| 分类号 |
F01D5/18 |
主分类号 |
F01D5/18 |
| 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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