发明名称 |
TURBINE AIRFOIL FOR GAS TURBINE ENGINE |
摘要 |
A hollow cooled turbine airfoil (18) is provided having pressure and suction side walls (20, 22) and a plurality of trailing edge cooling passages (46) that feed cooling air bleed slots (28) at the trailing edge (26). The trailing edge (26) is selectively thickened in the root (34) portion so as to allow shortened trailing edge slots (28), thereby improving trailing edge (26) cooling and reducing mechanical and thermal stresses.
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申请公布号 |
CA2398502(A1) |
申请公布日期 |
2003.02.28 |
申请号 |
CA20022398502 |
申请日期 |
2002.08.15 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
MCRAE, RONALD EUGENE JR.;TIMKO, LAWRENCE PAUL;FREY, DAVID ALAN;LEEKE, LESLIE EUGENE;KEITH, SEAN ROBERT |
分类号 |
F01D5/18;(IPC1-7):F01D5/14 |
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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