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Degradation mechanism for high temperature erosion in surface modified IN718 superalloy

机译:表面改性IN718高温合金的高温腐蚀降解机理

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Nickel based superalloy, Inconel 718, is one of the main candidates for high temperature applications such as air craft, land base and marine turbines. This technical paper deals with high temperature erosion behaviour and its mechanism of Al2O3-40TiO(2) (A40T) coating on Inconel 718 alloy. Al2O3-40TiO(2) coatings through plasma spray method were made on Inconel 718. The erosion behaviour of the A40T coating was studied using hot air jet erosion experiments at 800 degrees C with varying parameters like angle of impingement and erodent velocity. Characterisation of the samples was carried out using SEM images, and mechanisms of erosion are discussed. Images (SEM) reveal that the A40T coating exhibit ductile and brittle behaviour by ploughing and network cracking with grain chipping at 45 degrees angle of impingement, while at 90 degrees, it is brittle behaviour by network cracking and grain ejection. This investigation concludes that A40T coating on IN718 provides good erosion resistance at elevated temperatures.
机译:镍基超合金Inconel 718是飞机,陆基和轮机等高温应用的主要候选材料之一。该技术论文探讨了Inconel 718合金上的Al2O3-40TiO(2)(A40T)涂层的高温腐蚀行为及其机理。在Inconel 718上通过等离子喷涂法制备了Al2O3-40TiO(2)涂层。使用热空气喷射腐蚀实验在800摄氏度下采用不同的参数(例如撞击角度和腐蚀速度)研究了A40T涂层的腐蚀行为。使用SEM图像对样品进行表征,并讨论了腐蚀机理。图像(SEM)显示,A40T涂层通过在45度的撞击角下进行崩裂和带有颗粒崩裂的网状裂纹而表现出延性和脆性,而在90度时,它通过网状裂纹和晶粒弹出而具有脆性。这项研究得出的结论是,IN718上的A40T涂层在高温下具有良好的抗腐蚀性能。

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