发明名称 TURBINE ENGINE COMPONENT AND MANUFACTURING METHOD
摘要 <P>PROBLEM TO BE SOLVED: To provide coating composition for preventing the durability of a coating used to provide insulation for metallic components operating at elevated temperatures from being affected by engine operating conditions. <P>SOLUTION: The turbine engine component comprises a substrate (12), a bond coat (14) applied to a surface of the substrate (12), a first ceramic layer (16) having a cracked structure applied on top of the bond coat (14), and a second ceramic layer (18) having a cracked structure applied on top of the first ceramic layer (16). <P>COPYRIGHT: (C)2008,JPO&INPIT
申请公布号 JP2008064089(A) 申请公布日期 2008.03.21
申请号 JP20070212138 申请日期 2007.08.16
申请人 UNITED TECHNOL CORP <UTC> 发明人 FRELING MELVIN;SCHLICHTING KEVIN W
分类号 F01D5/28;C23C4/02;C23C4/10;F02C7/00 主分类号 F01D5/28
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