发明名称 |
CERAMIC COVERED TURBINE COMPONENTS |
摘要 |
A component for a gas turbine engine comprises an underlying substrate. A plurality of ceramic panels have intermediate thermal expansion joints bonded by a bond layer to the underlying substrate. The thermal expansion joints are formed of a material having a greater coefficient of expansion than a material forming the ceramic panels. The ceramic panels and the thermal expansion joints are positioned to define an outer surface for the component. A gas turbine engine and a component for a gas turbine engine are also disclosed. |
申请公布号 |
EP3099912(A4) |
申请公布日期 |
2017.02.01 |
申请号 |
EP20150742745 |
申请日期 |
2015.01.05 |
申请人 |
United Technologies Corporation |
发明人 |
COOK, III Grant O.;TWELVES, Wendell V. |
分类号 |
F02C7/20;F01D5/14;F01D5/28;F01D25/24;F02C7/24 |
主分类号 |
F02C7/20 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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