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
| Title |
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 |
- Khajmberg Beate
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- Khoffmann Mikhael'
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- Khong Chu-Van
- Al'Dinger Fritts
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|
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1996 |
- Norbert Chekh
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|
RU2168558C2 |
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2004 |
|
RU2334022C2 |
| ALLOY, PROTECTIVE LAYER AND PART |
2010 |
|
RU2521924C2 |
| ALLOY, PROTECTIVE LAYER AND STRUCTURAL COMPONENT |
2011 |
- Shmitts,Fridkhel'M
- Shtamm,Verner
|
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| ALLOY, PROTECTIVE LAYER AND STRUCTURAL PART |
2012 |
|
RU2574559C2 |
| ALLOY, PROTECTIVE LAYER AND STRUCTURAL PART |
2011 |
- Shmitts,Fridkhel'M
- Shtamm,Verner
|
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
- Kajzer, Aksel
- Shtamm, Verner
- Shtajnbakh, Yan
- Tomaidis, Dimitrios
|
RU2597459C2 |
