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

机译:定向凝固镍高超合金热耐腐蚀性的评价

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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°C and 900°C (below and above the melting point of salt, 884°C). The results show scale morphology on material surface and changes in chemical composition of surface of nickel superalloy.
机译:由定向固化的镍基超合金制成的涡轮机叶片暴露于高温和排气烟雾的组合,其中出现耐硫,钠和钒(热腐蚀)等腐蚀促进元素。超合金的耐腐蚀性主要取决于它们的结构和化学组成。因此,重要的是要意识到热腐蚀与材料表面的化学成分和形态之间的相关性。下文提出了硫对定向凝固的镍基超合金的微观结构的影响。该研究在850℃和900℃的温度下在Na_2SO_4环境中进行(低于盐,884℃的熔点。结果表明了镍超合金表面材料表面的规模形态和变化。

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