方石英
材料科学
陶瓷
等温过程
氧化物
温度循环
涂层
微观结构
镱
冶金
复合材料
化学工程
硅酸盐
矿物学
化学
光电子学
兴奋剂
热的
气象学
工程类
热力学
物理
石英
作者
Kenneth Kane,Eugenio García,Michael J. Lance,Cory Parker,Sanjay Sampath,Bruce A. Pint
摘要
Abstract Environmental barrier coatings (EBCs) will be needed to protect SiC‐based ceramic matrix composite components for the next generation of high‐efficiency industrial gas turbines (IGTs). The IGT application will require ≥25 kh lifetimes, and little data are available on EBC failure mechanisms, particularly at ≥1300°C. Initial 1‐h furnace cycle testing at 1350°C in 90 vol% H 2 O/10 vol% air was conducted ≥1000 cycles on thermally sprayed ytterbium disilicate (YbDS) coatings with and without an Si bond coating. By ≥1000 h, both EBCs formed thick, highly cracked, and fully crystalline cristobalite scales. Comparison of thermally grown oxide (TGO) microstructure and kinetics to isothermal rates of Si and SiC steam oxidation indicated a departure from slow‐growing parabolic growth to more rapid rates of silica formation. Possible mechanisms and implications for this acceleration are discussed.
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