发明名称 |
LOW PERMEABILITY HIGH PRESSURE COMPRESSOR ABRADABLE SEAL FOR BARE NI AIRFOILS HAVING CONTINUOUS METAL MATRIX |
摘要 |
An air seal (60) in a gas turbine engine (10) comprising a substrate (40). A bond coating layer (65) is adhered to the substrate (40). An abradable layer (70) is adhered to the bond coating layer (65). The abradable layer (70) comprises a metal matrix discontinuously filled with a soft ceramic material. |
申请公布号 |
EP2937437(A1) |
申请公布日期 |
2015.10.28 |
申请号 |
EP20150164502 |
申请日期 |
2015.04.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
STROCK, CHRISTOPHER W. |
分类号 |
C23C4/00;F01D11/12 |
主分类号 |
C23C4/00 |
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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