发明名称 |
Turbine shroud segment transpiration cooling with individual cast inlet and outlet cavities |
摘要 |
A shroud segment of a turbine shroud of a gas turbine engine comprises a platform with front and rear legs. The platform defines a plurality of axially extending holes with individual inlets on an outer surface of the platform for transpiration cooling of the platform of the turbine shroud segment.
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申请公布号 |
US7520715(B2) |
申请公布日期 |
2009.04.21 |
申请号 |
US20050183741 |
申请日期 |
2005.07.19 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
DUROCHER ERIC;FARAH ASSAF |
分类号 |
F01D11/08 |
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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