发明名称 Method for machining a coated gas turbine blade
摘要 Roughness of the ceramic layer (3) applied to the base material (1) is reduced locally (5). Elsewhere (6), original roughness of the ceramic layer (3) is maintained. An Independent claim is included for a gas turbine component prepared as described.
申请公布号 EP1284337(B1) 申请公布日期 2005.04.06
申请号 EP20020405661 申请日期 2002.07.30
申请人 ALSTOM TECHNOLOGY LTD 发明人 ANDERSON, GORDON;FRIED, REINHARD;LOETZERICH, MICHAEL;OEHL, MARKUS;SCHLECHTRIEM, STEFAN;STENGELE, JOERG
分类号 F01D5/14;F01D5/28;(IPC1-7):F01D5/14;B64C21/10 主分类号 F01D5/14
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