| 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. |
| 申请公布号 |
CA2535140(C) |
申请公布日期 |
2014.06.03 |
| 申请号 |
CA20062535140 |
申请日期 |
2006.02.03 |
| 申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
SYNNOTT, REMY;DUROCHER, ERIC |
| 分类号 |
F01D5/14;F01D5/18 |
主分类号 |
F01D5/14 |
| 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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