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Evaluation of hot corrosion resistance of directionally solidified nickel-based superalloy

机译:定向凝固镍基高温合金的抗热腐蚀性能评估

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The turbine blades made of directionally solidified nickel-based superalloys are exposed to combination of high temperature and exhaust fumes, in which appear corrosion promoting elements like sulphur, sodium and vanadium (hot corrosion). Corrosion resistance of superalloys is mainly dependent on their structure and chemical composition. Therefore, it is important to be aware of the correlation between the hot corrosion and changes in chemical composition and morphology of a surface of the material. The following paper presents the influence of sulphur on the microstructure of directionally solidified nickel-based superalloy. The research was carried out in Na_2SO_4 environment at two temperatures of 850 ℃ and 900 ℃ (below and above the melting point of salt, 884℃). The results show scale morphology on material surface and changes in chemical composition of surface of nickel superalloy.
机译:由定向凝固的镍基高温合金制成的涡轮机叶片会暴露于高温烟气和排烟气中,其中会出现腐蚀促进元素,如硫,钠和钒(热腐蚀)。高温合金的耐腐蚀性主要取决于其结构和化学组成。因此,重要的是要意识到热腐蚀与材料表面化学成分和形态变化之间的相关性。以下论文介绍了硫对定向凝固镍基高温合金显微组织的影响。该研究是在Na_2SO_4环境中,分别在850℃和900℃(盐的熔点以下和以上884℃)两个温度下进行的。结果表明,材料表面的鳞片形态和镍合金表面化学成分的变化。

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