发明名称 |
SERPENTINE COOLING CIRCUIT AND METHOD FOR COOLING TIP SHROUD |
摘要 |
A serpentine cooling circuit is formed in a gas turbine blade to cool portions of the tip shroud, primarily the fillet between the airfoil and the tip shroud and the shroud edges.
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申请公布号 |
US2009304520(A1) |
申请公布日期 |
2009.12.10 |
申请号 |
US20060447910 |
申请日期 |
2006.06.07 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BRITTINGHAM ROBERT ALAN;WARD JOHN D. |
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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