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The influence of interfacial toughness, as influenced by sulfur and reactive elements, and stress on the cracking and spallation of alumina scales from metallic substrates.

机译:受硫和反应性元素影响的界面韧性和应力对金属基材上氧化铝鳞片的开裂和剥落的影响。

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摘要

Ni-based superalloys, such as single crystal PWA 1480 and 1484, are being used in aircraft engines as turbine blades and vanes. Fe-base alloys (FeCrAl) are used in automobiles (in catalytic converters) and in high temperature furnaces as heating elements. The protection of these alloys against oxidation is provided by the formation of a slow-growing alumina scale. The adherence of the alumina scale to the alloy is necessary to maintain the oxidation resistance under isothermal and cyclic conditions.; It has been established that small additions of reactive elements (Y, Hf and Ce) and removal of impurities such as sulfur from the alloy substantially improve the adherence of the alumina layer to the alloy. Despite a significant amount of research over the past 50 years, there is still much controversy regarding the detailed mechanisms responsible for the improvement of the adherence.; Following previous research reported in the literature, a program was carried out to investigate the factors which affect the adherence or cracking and spallation of protective alumina scale and how the reactive elements and sulfur content affect these factors for Ni-based superalloys (PWA 1480, 1484) and Fe-based alloys (FeCrAl, +Ti, +Y). New advanced techniques such as high resolution SEM, EDS, TEM, STEM, and XRD techniques have been employed to elucidate the "reactive element" and "sulfur" effects. Also, state of the art XRD equipment has been used to measure the strain or stress in the alumina scale at room temperature and at high temperature. The adhesion of the alumina scale to alloys was measured using indentation testing such as Rockwell C.; It was found that the major benefit of adding a reactive element is to tie up sulfur in the alloy and lower residual sulfur which is free to segregate to the alumina/alloy interface. Residual sulfur in the alloy diffuses to the intact alloy/alumina interfaces and voids, resulting in weakening of an otherwise strong interfacial bond.; Classical stress measurement techniques such as Tilting and Rocking techniques were modified with respect to the alumina. In addition, new techniques, the Fixed Incidence Multiplane (FIM) and the Fixed Incidence Tilting (FIT) techniques were developed and shown to be useful for thin oxide scales (t {dollar}<{dollar} 0.5 {dollar}mu{dollar}m thickness). Stresses (e.g. growth stresses) in alumina scales on FeCrAl alloys at 850-1100{dollar}spcirc{dollar}C were measured using the newly developed FIM technique. Until recently, growth stresses were thought to be negligible compared to the total residual stresses. Growth stresses measured in alumina scales on FeCrAl alloys at 1000{dollar}spcirc{dollar}C and 1100{dollar}spcirc{dollar}C were in the range of {dollar}-{dollar}1 GPa, which was higher than previously measured growth stresses. In situ stress measurement results indicated that growth stresses in alumina scales were still high in the presence of reactive elements (Y) and the addition of reactive element did not reduce growth stresses. Rather, it improves the adhesion of the alumina scale and prevents spalling of the alumina scale.
机译:镍基高温合金,例如单晶PWA 1480和1484,已在飞机发动机中用作涡轮叶片和叶片。铁基合金(FeCrAl)用于汽车(催化转化器)和高温炉中作为加热元件。这些合金的抗氧化保护是通过形成缓慢生长的氧化铝水垢来提供的。氧化铝鳞对合金的粘附是维持等温和循环条件下的抗氧化性所必需的。已经确定的是,少量添加反应性元素(Y,Hf和Ce)以及从合金中去除杂质例如硫会大大改善氧化铝层对合金的粘附性。尽管在过去的50年中进行了大量的研究,但是关于改善依从性的详细机制仍然存在很多争议。根据文献报道的先前研究,进行了一个程序来研究影响保护性氧化铝垢附着或破裂和剥落的因素,以及反应性元素和硫含量如何影响镍基高温合金的这些因素(PWA 1480、1484) )和铁基合金(FeCrAl,+ Ti,+ Y)。已经采用了诸如高分辨率SEM,EDS,TEM,STEM和XRD等新的先进技术来阐明“反应元素”和“硫”的作用。同样,现有技术的XRD设备已被用于在室温和高温下测量氧化铝鳞片中的应变或应力。氧化铝鳞片对合金的粘附力是使用压痕测试(例如Rockwell C.)测量的。已经发现,添加反应性元素的主要好处是可以束缚合金中的硫,并降低残留的硫,硫可以自由地偏析到氧化铝/合金界面。合金中残留的硫扩散到完整的合金/氧化铝界面和空隙中,从而削弱了原本牢固的界面键。相对于氧化铝,对诸如倾斜和摇摆技术之类的经典应力测量技术进行了改进。此外,还开发了新技术,即固定入射多平面(FIM)和固定入射倾斜(FIT)技术,它们对薄氧化皮非常有用(t {dollar} <{dollar} 0.5 {dollar} mu {dollar米厚度)。使用最新开发的FIM技术测量了850-1100 {sp} {dol}的FeCrAl合金上氧化铝鳞片上的应力(例如生长应力)。直到最近,与总残余应力相比,生长应力仍可以忽略不计。在FeCrAl合金上以氧化铝标度测量的生长应力在1000 1000spC dol和1100spspC the时处于1dolGPa的范围内,高于先前测得的值。增长压力。原位应力测量结果表明,在存在反应性元素(Y)的情况下,氧化铝鳞片上的生长应力仍然很高,并且添加反应性元素并不能降低生长应力。而是,它改善了氧化铝鳞片的粘附性并防止了氧化铝鳞片的剥落。

著录项

  • 作者

    Sarioglu, Cevat.;

  • 作者单位

    University of Pittsburgh.;

  • 授予单位 University of Pittsburgh.;
  • 学科 Engineering Materials Science.; Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1998
  • 页码 285 p.
  • 总页数 285
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;机械、仪表工业;
  • 关键词

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