发明名称 |
GAS TURBINE ENGINE CERAMIC COMPONENT ASSEMBLY AND BONDING |
摘要 |
A gas turbine engine component assembly includes a ceramic component having a first thermal characteristic. A metallic component has a second thermal characteristic. A bonding material secures the ceramic component to the metallic component. The bonding material includes at least one of a transient liquid phase bond and a partial transient liquid phase bond. The bonding material is configured to withstand a shear stress parameter relating to a differential between the first and second thermal characteristics. |
申请公布号 |
EP3022407(A4) |
申请公布日期 |
2017.03.22 |
申请号 |
EP20140826220 |
申请日期 |
2014.06.18 |
申请人 |
United Technologies Corporation |
发明人 |
COOK III, Grant O.;ABBOTT, Michael G.;MCCAFFREY, Michael G. |
分类号 |
F01D25/28;B32B37/12;C09J5/00;F01D25/08;F02C7/20;F02C7/24 |
主分类号 |
F01D25/28 |
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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