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The Evolution of Thermal Barrier Coatings in Gas Turbine Engine Applications

机译：燃气涡轮发动机应用中热障涂层的演变

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Layer Oxidation; Susan Manning Meier; Dinesh K. Gupta; Pratt Whitney;
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1. Thermal Barrier Coatings for Gas-Turbine Engine Applications [J] . Nitin P. Padture, Maurice Gell, Eric H. Jordan Science . 2002,第5566期

机译：燃气轮机应用的热障涂层
2. Layered, composite, and doped thermal barrier coatings exposed to sand laden flows within a gas turbine engine: Microstructural evolution, mechanical properties, and CMAS deposition [J] . Nieto Andy, Walock Michael, Ghoshal Anindya, Surface & Coatings Technology . 2018,第期

机译：层状，复合和掺杂热障涂层暴露于燃气轮机发动机内的砂载物流：微观结构演化，机械性能和CMAS沉积
3. Damage evolution in EB-PVD thermal barrier coatings for turbine blades in aircraft engines under close to reality testing conditions [J] . M.Bartsch, G.Marci, K.Mull International journal of materials & product technology . 2001,第1a2a3期

机译：在接近实际测试条件下，用于飞机发动机涡轮叶片的EB-PVD热障涂层的损伤演变
4. Non-destructive technique for measurement of thermal physical properties of thermal barrier coatings in gas turbine engine in the temperature range 500 ― 3000 K [C] . E. Litovsky, S. Horodetsky, J. Kleiman 41th Annual Conference of Metallurgists of CIM International Symposium on Aerospace Materials: Developments, Durability, Testing and Life Cycle Issues Aug 11-14, 2002 Montreal, Quebec, Canada . 2002

机译：测量温度范围为500〜3000 K的燃气轮机热障涂层热物理性能的无损技术
5. Gadolinia doped hafnia (Gd2O3- HfO 2) thermal barrier coatings for gas turbine applications. [D] . Gullapalli, Satya Kiran. 2014

机译：d掺杂的氧化f（Gd2O3- HfO 2）隔热涂层，用于燃气轮机应用。
6. Inaugural ArticleFrom the Cover: Atomic-scale insight and design principles for turbine engine thermal barrier coatings from theory [O] . Kristen A. Marino, Berit Hinnemann, Emily A. Carter 2011

机译：封面文章：理论上的涡轮发动机隔热涂层的原子尺度见解和设计原理
7. Influence of Isothermal Heat Treatment on Porosity and Crystallite Size in Axial Suspension Plasma Sprayed Thermal Barrier Coatings for Gas Turbine Applications [O] . Ashish Ganvir, Nicolaie Markocsan, Shrikant Joshi 2016

机译：等温热处理对燃气轮机轴向悬浮等离子喷涂热障涂层孔隙率和晶粒尺寸的影响

The Evolution of Thermal Barrier Coatings in Gas Turbine Engine Applications

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