热障涂层
材料科学
氧化钇稳定氧化锆
电子束物理气相沉积
锆酸盐
立方氧化锆
扫描电子显微镜
等温过程
衍射仪
热喷涂
复合材料
能量色散X射线光谱学
物理气相沉积
化学气相沉积
涂层
陶瓷
纳米技术
物理
钛酸酯
热力学
作者
Kadir Mert Döleker,Yasin Ozgurluk,Hayrettin Ahlatçı,Abdullah Cahit Karaoğlanlı
出处
期刊:Open Chemistry
[De Gruyter Open]
日期:2018-01-01
卷期号:16 (1): 986-991
被引量:19
标识
DOI:10.1515/chem-2018-0112
摘要
Abstract Thermal Barrier Coatings (TBCs) provide thermal insulation for gas turbine components operating at high temperatures. Generally, TBCs were produced on a MCrAlY bond coat with 7-8% Yttria Stabilized Zirconia (YSZ) using Atmospheric Plasma Spray (APS) technique. In this study, Inconel 718 substrate material was coated with CoNiCrAlY bond coat using high velocity oxygen fuel (HVOF) technique. Afterward, Gd 2 Zr 2 O 7 was deposited on samples using Electron Beam Physical Vapor Deposition (EB-PVD) technique. Produced TBCs were exposed to isothermal oxidation tests at 1000°C for 8 h, 24 h, 50 h and 100 h in muffle furnace. Scanning electron microscopy-energy distribution X-ray (SEM-EDX) spectroscopy was used to investigate thermally grown oxide (TGO) layer and TGO growth behavior of TBCs. In addition, X-ray Diffractometer (XRD) analysis was performed to TBCs to understand whether phase transformation occurs or not before and after oxidation.
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