发明名称 |
THERMAL PROTECTION COATING FOR A TURBINE-ENGINE PART, AND A METHOD OF MAKING IT |
摘要 |
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. |
申请公布号 |
US2012107110(A1) |
申请公布日期 |
2012.05.03 |
申请号 |
US201013380952 |
申请日期 |
2010.07.01 |
申请人 |
ARANTES ANTONIO CREMILDO;DUDON LAURENT PAUL;MONS CLAUDE MARCEL;SNECMA |
发明人 |
ARANTES ANTONIO CREMILDO;DUDON LAURENT PAUL;MONS CLAUDE MARCEL |
分类号 |
F04D29/44;B32B3/02;B32B5/16;B32B5/18;B32B15/04;C23C4/04;E04B1/74 |
主分类号 |
F04D29/44 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|