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Hafnium silicate/ytterbium silicate superhigh-temperature environmental barrier coating and preparation method thereof
The invention relates to the technical field of high-temperature protective coatings, in particular to a hafnium silicate/ytterbium silicate ultrahigh-temperature environmental barrier coating and a preparation method thereof.A hafnium silicate bonding layer, an ytterbium disilicate transition layer and an ytterbium monosilicate working top layer are sequentially deposited on the surface of a ceramic-based composite material matrix; the hafnium silicate/ytterbium silicate superhigh-temperature environmental barrier coating can enable a ceramic-based composite material hot end component to serve at a higher use temperature (higher than 1400 DEG C), and the superhigh-temperature environmental barrier coating system can be applied to the field of high-performance gas turbine engines, especially aero-engines. The ultrahigh-temperature environment barrier coating has high bonding strength, excellent coating interface stability and good water-oxygen and molten salt corrosion resistance, the heat efficiency of an engine is improved, the service life of the engine is prolonged, and the development trend of advanced aero-engines in the future to high thrust, high thrust-weight ratio, high heat efficiency and low emission is met.
本发明涉及高温防护涂层技术领域,具体涉及一种硅酸铪/硅酸镱超高温环境障涂层及其制备方法,在陶瓷基复合材料基体表面依次沉积硅酸铪粘结层、焦硅酸镱过渡层和单硅酸镱工作顶层,能使陶瓷基复合材料热端部件在更高使用温度(高于1400℃)下服役的一种硅酸铪/硅酸镱超高温环境障涂层,该超高温环境障涂层体系可应用于高性能燃气涡轮发动机领域,特别是航空发动机。本发明的超高温环境障涂层不仅具有高的结合强度、优异的涂层界面稳定性、良好的抗水氧和熔盐腐蚀性能,有利于提高发动机的热效率和使役寿命,满足未来先进航空发动机向大推力、高推重比、高热效率和低排放的发展趋势。
Hafnium silicate/ytterbium silicate superhigh-temperature environmental barrier coating and preparation method thereof
The invention relates to the technical field of high-temperature protective coatings, in particular to a hafnium silicate/ytterbium silicate ultrahigh-temperature environmental barrier coating and a preparation method thereof.A hafnium silicate bonding layer, an ytterbium disilicate transition layer and an ytterbium monosilicate working top layer are sequentially deposited on the surface of a ceramic-based composite material matrix; the hafnium silicate/ytterbium silicate superhigh-temperature environmental barrier coating can enable a ceramic-based composite material hot end component to serve at a higher use temperature (higher than 1400 DEG C), and the superhigh-temperature environmental barrier coating system can be applied to the field of high-performance gas turbine engines, especially aero-engines. The ultrahigh-temperature environment barrier coating has high bonding strength, excellent coating interface stability and good water-oxygen and molten salt corrosion resistance, the heat efficiency of an engine is improved, the service life of the engine is prolonged, and the development trend of advanced aero-engines in the future to high thrust, high thrust-weight ratio, high heat efficiency and low emission is met.
本发明涉及高温防护涂层技术领域,具体涉及一种硅酸铪/硅酸镱超高温环境障涂层及其制备方法,在陶瓷基复合材料基体表面依次沉积硅酸铪粘结层、焦硅酸镱过渡层和单硅酸镱工作顶层,能使陶瓷基复合材料热端部件在更高使用温度(高于1400℃)下服役的一种硅酸铪/硅酸镱超高温环境障涂层,该超高温环境障涂层体系可应用于高性能燃气涡轮发动机领域,特别是航空发动机。本发明的超高温环境障涂层不仅具有高的结合强度、优异的涂层界面稳定性、良好的抗水氧和熔盐腐蚀性能,有利于提高发动机的热效率和使役寿命,满足未来先进航空发动机向大推力、高推重比、高热效率和低排放的发展趋势。
Hafnium silicate/ytterbium silicate superhigh-temperature environmental barrier coating and preparation method thereof
一种硅酸铪/硅酸镱超高温环境障涂层及其制备方法
BIAN QING (Autor:in) / XUE ZHAOLU (Autor:in) / MEI JIAO (Autor:in) / LIU QINQIN (Autor:in) / ZHENG YUE (Autor:in)
10.09.2024
Patent
Elektronische Ressource
Chinesisch
IPC:
C04B
Kalk
,
LIME
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