UEC Showcases Electron-Beam Evaporation Method for Applying Thermal Barrier Coating to Gas Turbine Engine Blades for the First Time

The coating thickness does not exceed two human hairs in cross-section

United Engine Corporation (UEC) showed in a video the process of applying a thermal barrier coating to gas turbine engine blades using the electron-beam evaporation method.

Ceramic coating — yttria-stabilized zirconia (YSZ), allowing turbine blades to operate in a high-speed gas flow. To coat the blades with the thinnest layer of ceramic coating, the material is evaporated with a high-power electron beam, while the blades rotate in the resulting vapor.

The coating thickness does not exceed 0.15 mm — approximately 2-3 human hairs in cross-section. Coating the blades with yttria-stabilized zirconia improves the heat resistance of the parts.

This is necessary to maintain the integrity of the blades, as the gas flow temperature can reach 1800-2000 degrees Celsius, which exceeds the melting point of the metal from which the turbine blades are made.

Earlier www1.ru reported that 200 aircraft will be built in Russia by 2030: there are guaranteed buyers with money.

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