发明名称 Turbine engine component having enhanced heat transfer characteristics and method for forming same
摘要 <p>A turbine engine component (10) is provided that has a surface that contains a plurality of depressions (21) that are effective to increase the surface area of the component. The depressions are generally concave in contour and improve the heat transfer characteristics of the component. Methods for forming the turbine engine components are also disclosed. <IMAGE></p>
申请公布号 EP1065345(A2) 申请公布日期 2001.01.03
申请号 EP20000305461 申请日期 2000.06.29
申请人 GENERAL ELECTRIC COMPANY 发明人 HASZ, WAYNE CHARLES;ABUAF, NESIM;JOHNSON, ROBERT ALAN;LEE, CHING-PANG
分类号 F01D5/14;B22C9/10;B22C9/22;B22C9/24;B22D25/02;B23K1/00;F01D5/18;F01D5/28;F01D25/08;F02C7/00;F28F13/18;F28F21/08;(IPC1-7):F01D5/18 主分类号 F01D5/14
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