发明名称 |
Blade tip cooling |
摘要 |
<p>A turbine blade includes a hollow airfoil having a squealer tip rib (36) extending outboard from a tip cap (40) enclosing the airfoil. An impingement baffle (44) is spaced inboard from the tip cap to define a tip plenum (46) therebetween. Impingement holes (48) extend through the baffle and are directed at the junction (42) of the rib and cap for impinging a coolant jet thereagainst. <IMAGE></p> |
申请公布号 |
EP1079072(A2) |
申请公布日期 |
2001.02.28 |
申请号 |
EP20000305652 |
申请日期 |
2000.07.05 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
CORREIA, VICTOR HUGO SILVA;MANNING, ROBERT FRANCIS |
分类号 |
F01D5/18;F01D5/20;(IPC1-7):F01D5/20 |
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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