FIELD: metallurgy.
SUBSTANCE: invention relates to the field of metallurgy and can be used for parts operating simultaneously under wear and impact of conditions of corrosive media, namely for nozzle blades of gas turbine engines that are affected by high-speed gas flows, sudden temperature changes, erosion and corrosion, and air and space vehicles experiencing impact of incoming flow of dissociated air in the atmosphere at speed above 2,000 m/s. Two-layer heat-resistant coating on products made of carbon-carbon composite materials contains heat-resistant sub-layer and outer layer of stabilized zirconia (ZrO2-Y2O3), while sub-layer is made of nickel alloy Ni23Co20Cr8AlY, and outer layer additionally contains molybdenum disilicide (MoSi2) with the following component ratio, wt.%: stabilized zirconia (ZrO2-Y2O3) – 10–20, molybdenum disilicide (MoSi2) – the rest, with outer coating layer (MoSi2-ZrO2-Y2O3) having thickness of 250–300 mcm, and sublayer (Ni23Co20Cr8AlY) – 20–40 mcm.
EFFECT: invention is directed to coating having self-healing effect and to reducing thermal stresses of coating layers.
1 cl, 1 ex, 2 tbl
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Authors
Dates
2018-07-26—Published
2017-05-30—Filed