发明名称 |
HEAT-PROTECTIVE COATING FOR A TURBINE ENGINE PART, AND METHOD FOR PRODUCING SAME |
摘要 |
<p>A thermal protection coating, in particular for a turbine-engine part (12), the coating being deposited by thermal spraying onto the surface of the part (12) and including at least 80% by volume of hollow ceramic microbeads distributed in a metal alloy based on nickel or cobalt, it being possible for the coating to be deposited on a bonding layer (22) of metal alloy and for it to be covered in a layer (26) providing protection against erosion or against friction wear, or in a reflective layer that reflects thermal radiation.</p> |
申请公布号 |
EP2449146(A1) |
申请公布日期 |
2012.05.09 |
申请号 |
EP20100742020 |
申请日期 |
2010.07.01 |
申请人 |
SNECMA |
发明人 |
ARANTES, ANTONIO, CREMILDO;DUDON, LAURENT, PAUL;MONS, CLAUDE, MARCEL |
分类号 |
C23C4/02;C23C4/06;C23C28/00 |
主分类号 |
C23C4/02 |
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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