FIELD: protective coatings. SUBSTANCE: protective layer, in particular, for protection of gas turbine parts, contains ceramic insulation layer and adhesive layer of rhenium-containing metal alloy defined by general formula MCrAlY wherein M is cobalt and/or nickel and Y yttrium and/or at least one equivalent metal selected from scandium and rare-earth metals. EFFECT: increased oxidation, corrosion, and temperature resistance. 10 cl
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Year |
Author |
Number |
| ARTICLE FOR DIRECTION OF HOT OXIDIZING GAS |
1996 |
|
RU2149202C1 |
| A GAS TURBINE MEMBER (VERSIONS) AND METHOD TO MANUFACTURE ITS HEAT-INSULATING COATING |
1998 |
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2004 |
|
RU2334022C2 |
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1996 |
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|
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2010 |
|
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2011 |
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2012 |
|
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2011 |
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|
RU2562656C2 |
| PROTECTIVE COAT FOR COMPONENTS SUBJECTED TO EROSION-CORROSION ACTION IN HIGH-TEMPERATURE MEDIUM |
1996 |
|
RU2167220C2 |
| SYSTEM OF LAYERS WITH DOUBLE METAL MCrAlY-COATING |
2011 |
- Bostanjoglo, Georg
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- Shtajnbakh, Yan
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|
RU2597459C2 |
