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Hot corrosion of cobalt chromium aluminum yttrium alloys.

机译:钴铬铝钇合金的热腐蚀。

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摘要

The kinetics and mechanisms of the hot corrosion of CoCrAlY alloys over wide ranges of temperature (600-1000{dollar}spcirc{dollar}C) and Pso{dollar}sb3{dollar} (10{dollar}sp{lcub}-6{rcub}{dollar}-10{dollar}sp{lcub}-3{rcub}{dollar} atm) were studied. Isothermal and cyclic experiments were performed to study the kinetics, and microstructures were examined by scanning electron microscopy. After interpreting these results, the hot corrosion mechanisms of the CoCrAlY alloys were proposed to explain the observed behavior.; The reaction mechanism governing hot corrosion is thought to be as follows. At low temperature (600-800{dollar}spcirc{dollar}C), SO{dollar}sb3{dollar} and CoO react and form a molten Na{dollar}sb2{dollar}SO{dollar}sb4{dollar}-CoSO{dollar}sb4{dollar} salt mixture. Aluminum diffuses through the alloy, is oxidized, and the alumina which is formed becomes subject to basic fluxing. While alumina is subject to the Rapp-Goto mechanism, chromia may not be subject to this mechanism. Since Co is left behind in the alloy, the basic fluxing of alumina seems to be the cause for formation of nonprotective scales. Sulfides can form during low temperature hot corrosion and considerable sulfide formation is observed at 800-850{dollar}spcirc{dollar}C, but the sulfidation process is less likely to be the major cause of LTHC. Also, the sulfite formation mechanism is evaluated, and the activity of aluminum sulfite is found to be too low for this compound to exist. At high temperature (900-1000{dollar}spcirc{dollar}C), the CoCrAlY alloy was in the initiation stage due to the formation of protective alumina during isothermal tests.; The mode of degradation of the CoCrAlY alloy at 1000{dollar}spcirc{dollar}C in pure oxygen during the cyclic tests was basic fluxing of alumina and chromia accompanied by spalling and cracking of oxides.
机译:CoCrAlY合金在宽温度范围(600-1000 {dol} spcirc {dollar} C)和Pso {dollar} sb3 {dollar(10 {dollar} sp {lcub} -6 { rcub} {dollar} -10 {dollar} sp {lcub} -3 {rcub} {dollar} atm)。进行等温和循环实验以研究动力学,并且通过扫描电子显微镜检查微观结构。在解释了这些结果之后,提出了CoCrAlY合金的热腐蚀机理来解释观察到的行为。认为控制热腐蚀的反应机理如下。在低温(600-800 {dollar} spcirc {dollar} C)下,SO {dollar} sb3 {dollar}和CoO反应并形成熔融的Na {dollarssb2 {dollar} SO {dollar} sb4 {dollar} -CoSO {dolb} sb4 {dollar}盐混合物。铝扩散通过合金,被氧化,形成的氧化铝经受碱性助熔剂作用。尽管氧化铝受Rapp-Goto机制影响,但氧化铬可能不受此机制影响。由于Co残留在合金中,因此氧化铝的基本助熔剂似乎是形成非保护性水垢的原因。在低温热腐蚀过程中会形成硫化物,在800-850℃时会观察到大量硫化物的形成,但硫化过程不太可能是LTHC的主要原因。另外,评估了亚硫酸盐的形成机理,发现亚硫酸铝的活性太低,以致于该化合物不存在。在高温下(900-1000spC),由于在等温试验中形成了保护性氧化铝,CoCrAlY合金处于起爆阶段。在循环试验中,CoCrAlY合金在纯氧中于1000 spC循环降解的方式是氧化铝和氧化铬的基本通量,以及氧化物的剥落和裂化。

著录项

  • 作者

    Hwang, Soon Young.;

  • 作者单位

    University of Pittsburgh.;

  • 授予单位 University of Pittsburgh.;
  • 学科 Engineering Metallurgy.; Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 1989
  • 页码 162 p.
  • 总页数 162
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 冶金工业;工程材料学;
  • 关键词

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