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
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