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The primary creep behavior of single crystal, nickel base superalloys PWA 1480 and PWA 1484.

机译:单晶镍基高温合金PWA 1480和PWA 1484的主要蠕变行为。

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摘要

Primary creep occurring at intermediate temperatures (650°C to 850°C) and loads greater than 500 MPa has been shown to result in severe creep strain, often exceeding 5-10%, during the first few hours of creep testing. This investigation examines how the addition of rhenium and changes in aging heat treatment affect the primary creep behavior of PWA 1480 and PWA 1484. To aid in the understanding of rhenium's role in primary creep, 3wt% Re was added to PWA 1480 to create a second generation version of PWA 1480. The age heat treatments used for creep testing were either 704°C/24 hr. or 871°C/32hr. All three alloys exhibited the presence of secondary gamma' confirmed by scanning electron microscopy and local electrode atom probe techniques. These aging heat treatments resulted in the reduction of the primary creep strain produced in PWA 1484 from 24% to 16% at 704°C/862 MPa and produced a slight dependence of the tensile properties of PWA 1480 on aging heat treatment temperature.;For all test temperatures, the high temperature age resulted in a significant decrease in primary creep behavior of PWA 1484 and a longer lifetime for all but the lowest test temperature. The primary creep behavior of PWA 1480 and PWA 1480+Re did not display any significant dependence on age heat treatment. The creep rupture life of PWA 1480 is greater than PWA 1484 at 704°C, but significantly shorter at 760°C and 815°C. PWA 1480+Re, however, displayed the longest lifetime of all three alloys at both 704°C and 815°C (PWA 1480+Re was not tested at 760°C). Qualitative TEM analysis revealed that PWA 1484 deformed by large dislocation "ribbons" spanning large regions of material. PWA 1480, however, deformed primarily due to matrix dislocations and the creation of interfacial dislocation networks between the gamma and gamma' phases. PWA 1480+ contained stacking faults as well, though they acted on multiple slip systems generating work hardening and forcing the onset of secondary creep. X-ray diffraction and JMatPro calculations were also used to gain insight into the cause of the differences in behaviors.
机译:在蠕变测试的最初几个小时内,发生在中间温度(650°C至850°C)且载荷大于500 MPa的一次蠕变已表明会导致严重的蠕变应变,通常超过5-10%。这项调查研究了the的添加和时效热处理的变化如何影响PWA 1480和PWA 1484的主要蠕变行为。为帮助理解of在主要蠕变中的作用,向PWA 1480中添加了3wt%的Re,以创建a新一代版本的PWA1480。用于蠕变测试的时效热处理为704°C / 24小时。或871°C / 32hr。所有三种合金均显示出通过扫描电子显微镜和局部电极原子探针技术证实存在次生γ'。这些老化的热处理导致PWA 1484在704°C / 862 MPa下产生的一次蠕变应变从24%降低到16%,并且使PWA 1480的拉伸性能与老化热处理温度略有相关。在所有测试温度下,高温老化导致PWA 1484的主要蠕变行为显着降低,并且除了最低测试温度外,所有其他寿命都更长。 PWA 1480和PWA 1480 + Re的主要蠕变行为对老化热处理没有明显的依赖性。在704°C时,PWA 1480的蠕变断裂寿命大于PWA 1484,但在760°C和815°C时则显着缩短。但是,PWA 1480 + Re在704°C和815°C下均表现出所有三种合金的最长寿命(未在760°C下测试PWA 1480 + Re)。定性TEM分析显示,PWA 1484因跨大面积材料的大位错“色带”而变形。然而,PWA 1480主要由于基体位错和在γ相与γ'相之间形成界面错位网络而变形。 PWA 1480+也包含堆叠故障,尽管它们作用于多个滑移系统上,从而导致工作硬化并迫使二次蠕变开始。 X射线衍射和JMatPro计算也被用来深入了解行为差异的原因。

著录项

  • 作者

    Wilson, Brandon Charles.;

  • 作者单位

    University of Florida.;

  • 授予单位 University of Florida.;
  • 学科 Engineering Metallurgy.;Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2008
  • 页码 297 p.
  • 总页数 297
  • 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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