FIELD: metallurgy.
SUBSTANCE: protective coating of a gas turbine component contains, by weight %: Co 15-39, Cr 10-25, Al 5-15, Y 0.05-1, Fe 0.5-10, Mo 0.05-2, nickel and impurities are the rest.
EFFECT: high resistance to oxidation and corrosion.
8 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
SYSTEM OF LAYERS WITH DOUBLE METAL MCrAlY-COATING | 2011 |
|
RU2597459C2 |
BINDING METAL COATING WITH HIGH GAMMA/GAMMA' TRANSITION TEMPERATURE, AND COMPONENT | 2010 |
|
RU2521925C2 |
SYSTEM OF LAYERS WITH TWO-LAYER METAL LAYER | 2011 |
|
RU2566693C2 |
ALLOY, PROTECTIVE LAYER AND STRUCTURAL PART | 2011 |
|
RU2562656C2 |
METAL COATING WITH BINDER THAT FEATURES HIGH TEMPERATURE OF GAMMA/GAMMA' TRANSITION AND THE PART | 2010 |
|
RU2523185C2 |
ALLOY, PROTECTIVE LAYER AND STRUCTURAL PART | 2012 |
|
RU2574559C2 |
NANO- AND MICROSTRUCTURED CERAMIC THERMAL BARRIER COATING | 2010 |
|
RU2518850C2 |
LAYERED SYSTEM OF COATING WITH MCRALX LAYER AND CHROME-ENRICHED LAYER AND METHOD OF OBTAINING THEREOF | 2009 |
|
RU2542870C2 |
HONEYCOMB SEAL AND METHOD OF ITS MANUFACTURING | 2009 |
|
RU2515869C2 |
METHOD OF DEPOSITION OF PROTECTIVE COATINGS ON DETAILS MADE OUT OF REFRACTORY ALLOYS | 2000 |
|
RU2264480C2 |
Authors
Dates
2017-09-25—Published
2014-04-22—Filed