Corrosion resistant plasma sprayed (Y0.8Gd0.2)3Al5O12/YSZ thermal barrier coatings towards molten calcium-magnesium-alumina-silicate

作者: Shiyu Sun , Zhaolu Xue , Wenting He , Jian He , Qiushi Li

DOI: 10.1016/J.CERAMINT.2019.01.114

关键词:

摘要: Abstract Chemical reaction between (Y 0.8 Gd 0.2) 3 Al 5 O 12 (GYAG) and calcium-magnesium-alumina-silicate (CMAS) with four different compositions was investigated. The GYAG revealed excellent chemical stability with molten CMAS even after 24 h heat-treatment at 1250° C. A GYAG layer was sprayed onto an yttria stabilized zirconia (YSZ) thermal barrier coating (TBC) by plasma spray and the thermal cycling behavior and resistance to CMAS corrosion of the coating system were researched. The GYAG/YSZ TBC …

参考文章(27)
Xin Zhou, Binglin Zou, Limin He, Zhenhua Xu, Jiaying Xu, Rende Mu, Xueqiang Cao, Hot corrosion behaviour of La2(Zr0.7Ce0.3)2O7 thermal barrier coating ceramics exposed to molten calcium magnesium aluminosilicate at different temperatures Corrosion Science. ,vol. 100, pp. 566- 578 ,(2015) , 10.1016/J.CORSCI.2015.08.031
G. S. Ccorman, High‐Temperature Creep of Some Single Crystal Oxides John Wiley & Sons, Inc.. pp. 1745- 1766 ,(2008) , 10.1002/9780470313848.CH10
Stephan Krämer, James Yang, Carlos G. Levi, Infiltration-Inhibiting Reaction of Gadolinium Zirconate Thermal Barrier Coatings with CMAS Melts Journal of the American Ceramic Society. ,vol. 91, pp. 576- 583 ,(2008) , 10.1111/J.1551-2916.2007.02175.X
Philipp H. Klein, William J. Croft, Thermal Conductivity, Diffusivity, and Expansion of Y2O3, Y3 Al5O12, and LaF3 in the Range 77°–300°K Journal of Applied Physics. ,vol. 38, pp. 1603- 1607 ,(1967) , 10.1063/1.1709730
Xun Zhan, Zhen Li, Bin Liu, Jingyang Wang, Yanchun Zhou, Zijun Hu, Theoretical Prediction of Elastic Stiffness and Minimum Lattice Thermal Conductivity of Y3Al5O12, YAlO3 and Y4Al2O9 Journal of the American Ceramic Society. ,vol. 95, pp. 1429- 1434 ,(2012) , 10.1111/J.1551-2916.2012.05118.X
David R. Clarke, Matthias Oechsner, Nitin P. Padture, Thermal-barrier coatings for more efficient gas-turbine engines Mrs Bulletin. ,vol. 37, pp. 891- 898 ,(2012) , 10.1557/MRS.2012.232
Wolfgang Braue, Peter Mechnich, Recession of an EB-PVDYSZ Coated Turbine Blade by CaSO4 and Fe, Ti-Rich CMAS-Type Deposits Journal of the American Ceramic Society. ,vol. 94, pp. 4483- 4489 ,(2011) , 10.1111/J.1551-2916.2011.04747.X
Jing Wu, Hong-bo Guo, Yu-zhi Gao, Sheng-kai Gong, Microstructure and thermo-physical properties of yttria stabilized zirconia coatings with CMAS deposits Journal of The European Ceramic Society. ,vol. 31, pp. 1881- 1888 ,(2011) , 10.1016/J.JEURCERAMSOC.2011.04.006
R. A. Miller, Thermal barrier coatings for aircraft engines: History and directions Journal of Thermal Spray Technology. ,vol. 6, pp. 35- 42 ,(1997) , 10.1007/BF02646310
Nitin P Padture, Maurice Gell, Eric H Jordan, Thermal Barrier Coatings for Gas-Turbine Engine Applications Science. ,vol. 296, pp. 280- 284 ,(2002) , 10.1126/SCIENCE.1068609