发明名称 |
COATING SYSTEM FOR A GAS TURBINE COMPONENT |
摘要 |
A system or method for applying a protective environmental coating for a gas turbine component. The coating includes a bond layer applied to a substrate comprised of a ceramic matrix composite material and environmental barrier coating layers. The first environmental barrier coating layer is bonded to the substrate by the bond layer. The bond layer comprises silicon and particles consisting of particles of Lanthanum or Cerium. |
申请公布号 |
US2014011038(A1) |
申请公布日期 |
2014.01.09 |
申请号 |
US201213542184 |
申请日期 |
2012.07.05 |
申请人 |
DAS RUPAK;SCHAEFFER JON CONRAD;ZHANG JAMES;GENERAL ELECTRIC COMPANY |
发明人 |
DAS RUPAK;SCHAEFFER JON CONRAD;ZHANG JAMES |
分类号 |
B32B9/04;B05D3/02;C23C4/12;C23C16/44;C23C16/48 |
主分类号 |
B32B9/04 |
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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