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The current paper explains the oxidation behaviour of a newly developed nickel-based superalloy in simulating aero gas turbine engine conditions. The results showed that the new superalloy is highly susceptible to high temperature oxidation. Within three of hours of oxidation, extensive oxide scales were formed. The formed oxide scales were ana-lysed with electron dispersive spectroscopy (EDS) and morphology was studied with scanning electron microscope (SEM) for varied oxidation times. The oxidation products were determined with XRD and cross sections of all the oxi-dised superalloys were also studied. The elemental distribution of all the superalloys after oxidation was also studied with a view to understand and compare the characteristics of the new superalloy with other superalloys. Finally, an oxidation mechanism that is responsible for its faster degradation under elevated temperatures was established based on the results obtained with different techniques and presented in detail.
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篇名 Oxidation Behaviour of a Newly Developed Superalloy
来源期刊 表面工程材料与先进技术期刊(英文) 学科 医学
关键词 Gas TURBINE Engine Components SUPERALLOYS High Temperature OXIDATION
年,卷(期) bmgcclyxjjsqkyw_2011,(3) 所属期刊栏目
研究方向 页码范围 130-135
页数 6页 分类号 R73
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研究主题发展历程
节点文献
Gas
TURBINE
Engine
Components
SUPERALLOYS
High
Temperature
OXIDATION
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研究来源
研究分支
研究去脉
引文网络交叉学科
相关学者/机构
期刊影响力
表面工程材料与先进技术期刊(英文)
季刊
2161-4881
武汉市江夏区汤逊湖北路38号光谷总部空间
出版文献量(篇)
211
总下载数(次)
0
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