发明名称 CERAMIC MATRIX COMPOSITE COMPONENT, TURBINE SYSTEM AND FABRICATION PROCESS
摘要 <p>PROBLEM TO BE SOLVED: To provide a turbine excellent in efficiency and performance.SOLUTION: A ceramic matrix composite component, a turbine system and a fabrication process are disclosed. The ceramic matrix composite (CMC) component includes a CMC material, an environmental barrier coating (EBC) on the CMC material, and a hard wear-resistant coating applied over the EBC. The turbine system includes a rotatable CMC component having a hard wear-resistant coating, and a stationary turbine component, the stationary turbine component having an abradable coating arranged to be cut by a silicon carbide material. A fabrication process includes positioning the rotatable CMC a pre-determined distance from the stationary turbine component, and rotating the rotatable CMC component. The hard wear-resistant coating on the rotatable CMC component cuts into the abradable coating on the stationary turbine component.</p>
申请公布号 JP2015067535(A) 申请公布日期 2015.04.13
申请号 JP20140194554 申请日期 2014.09.25
申请人 GENERAL ELECTRIC CO <GE> 发明人 DELVAUX JOHN MCCONNELL
分类号 C04B41/89;C23C14/06;C23C16/42;F01D5/08;F01D5/28;F01D9/04;F01D11/08;F01D25/00;F02C7/00 主分类号 C04B41/89
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