发明名称 Striated cooling hole
摘要 <p>A turbine airfoil (14) includes pressure and suction sides (22, 24) extending longitudinally from root (26) to tip (28), and chordally between leading and trailing edges (30, 32). A striated discharge hole (38) terminates outside the airfoil for discharging coolant therefrom. <IMAGE></p>
申请公布号 EP1098068(A2) 申请公布日期 2001.05.09
申请号 EP20000309704 申请日期 2000.11.02
申请人 GENERAL ELECTRIC COMPANY 发明人 SHAW, JAMES STEPHEN;FLECK, JAMES NORWOOD
分类号 B23H9/10;F01D5/18;F01D9/02;(IPC1-7):F01D5/18;B23H9/16;B23H9/14;B23H3/00 主分类号 B23H9/10
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