FIELD: mechanical engineering.
SUBSTANCE: invention relates to coatings to protect parts of exhaust system of gliders made from heat-resistant alloys and corrosion-resistant steels against high-temperature gas corrosion under operation at temperatures up to 600°C. Coating contains, wt %: SiO2 20.0-36.5, B2O3 4.0-5.0, Al2O3 5.0-6.0, BaO 5.0-6.0, CaO 2.0-4.0, MgO 0.5-1.5, TiO2 1.5-2.5, Cr2O3 15.0-17.0, Na2O 0.6-0.7, P2O5 0.5-1.5, sodium liquid glass 23.0-27.0, and mineral silica-based complex compound 5.0-6.0 composed of, wt %: SiO2 56.25-58.05, Al2O3 34.3-35.1, CaO 1.0-1.2, MgO 1.0-1.1, K2O 2.5-2.6, Na2O 0.6-0.7, TiO2 1.6-1.8, SO3 0.15-0.25, Fe2O3 0.8-1.0, or, instead of SiO2 56.25-58.05, SiO2 35.25-40.05 and SiB4 18.0-21.0. Reliability of operation with thus coated parts is increased by a factor of 1.5-2.
EFFECT: increased heat resistance and adhesion strength.
3 tbl
Title | Year | Author | Number |
---|---|---|---|
REFRACTORY COATING | 2002 |
|
RU2239616C2 |
HEAT-RESISTANT COVER | 2000 |
|
RU2191165C2 |
HEAT-RESISTANT COATING | 2006 |
|
RU2328472C1 |
HEAT-RESISTANT COATING | 2007 |
|
RU2358925C1 |
HEAT-RESISTANT COATING | 2004 |
|
RU2273609C1 |
HEAT-RESISTANT COVER | 2015 |
|
RU2598657C1 |
HEAT-RESISTANT COATING | 1999 |
|
RU2163897C2 |
HEAT-RESISTANT COVER | 2017 |
|
RU2661942C1 |
HEAT-RESISTANT MULTIFUNCTIONAL COATING | 2023 |
|
RU2812460C1 |
STEEL LINING | 2001 |
|
RU2230712C2 |
Authors
Dates
2005-06-27—Published
2003-11-26—Filed