发明名称 |
Cooled turbine blade |
摘要 |
A cooled turbine blade comprising a platform and an aerofoil portion has a rebate formed in the aerofoil portion near the trailing edge on the pressure face side. This rebate extends from the platform to the blade tip, and slots for the escape of cooling air from an internal cavity of the aerofoil portion open into the rebate.
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申请公布号 |
US6328531(B1) |
申请公布日期 |
2001.12.11 |
申请号 |
US19990412759 |
申请日期 |
1999.10.05 |
申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" |
发明人 |
BARIAUD CHRISTIAN BERNARD;BIL ERIC STéPHAN |
分类号 |
F01D5/14;F01D5/18;(IPC1-7):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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