发明名称 |
Turbine airfoil platform cooling core |
摘要 |
A gas turbine engine component (24) has a platform (28) and an airfoil (30) extending from the platform (28). The platform (28) has a pressure side (30) and a suction side (50). A cooling passage (34) is formed within the platform (28), and extends along the pressure side (32) of the platform (28). Air leaves the passage through an air outlet (40) on the suction side (50) of the platform (28). |
申请公布号 |
EP2325439(A2) |
申请公布日期 |
2011.05.25 |
申请号 |
EP20100251976 |
申请日期 |
2010.11.22 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BEATTIE, JEFFREY S.;GLEINER, MATTHEW S.;DEVORE, MATTHEW A.;JENNE, DOUGLAS C. |
分类号 |
F01D5/08;F01D5/18;F01D9/02 |
主分类号 |
F01D5/08 |
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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