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Use of Indentation Fracture Tests to Investigate Toughness Loss Mechanisms in Thermal Barrier Coating Systems

机译:使用压痕裂缝试验研究热屏障涂层系统中的韧性损失机制

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Loss of adhesion is a major concern in thermal barrier coating (TBC) systems used to insulate gas turbine components. Fracture mechanics-based indentation tests have been developed to quantify interfacial fracture toughness loss in electron beam physical vapor deposition (EB-PVD) TBC systems. Through the integration of indentation fracture test methods and electron microscope visualization techniques, the degradation of interfacial fracture toughness can be tracked quantitatively with thermal exposure history. In the present paper, the tracking of toughness loss and identification of the mechanisms causing it are demonstrated for TBCs subjected to isothermal dry air and cyclic dry air thermal exposures at 1100°C. Although tests to date have been on EB-PVD TBCs, the methods presented may also be applicable to other TBC systems.
机译:粘附损失是用于隔热燃气涡轮机部件的热障涂层(TBC)系统中的主要问题。已经开发出裂缝力学的压痕试验以量化电子束物理气相沉积(EB-PVD)TBC系统中的界面断裂韧性损失。通过缩进断裂试验方法和电子显微镜可视化技术的整合,可以用热暴露历史定量跟踪界面断裂韧性的劣化。在本文中,对在1100℃下进行等温干燥空气和环状干燥空气热曝光的TBC来证明韧性损失和导致其鉴定的跟踪。虽然测试日期已经在EB-PVD TBC上,但所提供的方法也可以适用于其他TBC系统。

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