| 发明名称 |
Apparatus and method for cooling a turbine shroud segment and vane outer shroud |
| 摘要 |
A cooling arrangement in a turbine section of gas turbine engines is used to direct cooling air within shroud segment platforms (44) for cooling the turbine shroud (32) while forming substantially straight cooling air streams for impingement cooling on a turbine vane outer shroud (38). |
| 申请公布号 |
EP1746254(B1) |
申请公布日期 |
2016.03.23 |
| 申请号 |
EP20060253774 |
申请日期 |
2006.07.19 |
| 申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
DUROCHER, ERIC;FARAH, ASSAF |
| 分类号 |
F01D11/08;F01D9/04;F01D25/12 |
主分类号 |
F01D11/08 |
| 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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