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Micromechanisms of quasi-static and fatigue crack growth in titanium-aluminides.

机译:钛铝化物准静态和疲劳裂纹扩展的微观机制。

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摘要

The rapid development of advanced aerospace technology has put an increasing demand on the development of a new generation of structural materials for aircraft engines. Intermetallics materials with low densities and improved fracture toughness at elevated temperature show promise for replacing widely used Ni-base superalloys. TiAl and Ti{dollar}sb3{dollar}Al, ordered intermetallic compounds of Ti and Al, have been the subject of increasing research activity in the recent past because of their light weight and high strength. An understanding of the resistance to quasi-static and cyclic load fracture in these intermetallics at both ambient and elevated temperatures is of paramount importance for damage-tolerant, fatigue-critical structural applications for which the intermetallics are candidate materials.; This thesis explores the effects of microstructure, microstructural stability, mechanical variables (such as load ratio and fatigue frequency), and temperature on the quasi-static and fatigue crack growth characteristics of Ti-Al and Ti-Al-Nb alloys. With the aid of controlled heat treatments, duplex microstructures comprising either {dollar}alphasb2{dollar} and {dollar}beta{dollar} or {dollar}alphasb2{dollar} and {dollar}gamma{dollar} phases as well as predominantly {dollar}alphasb2{dollar} phase microstructures are produced. The fatigue crack growth characteristics are monitered over a range of {dollar}Delta{dollar}K values from threshold to final failure. The effects of controlled microstructures on the overall fatigue and fracture resistance are examined in light of TEM observations of crack tip damage, scanning auger spectroscopy of fracture surface oxidation and scanning electron fractography. The stability of these microstructures are examined in light of their response to both fatigue crack growth and fracture toughness. Microstructural features which lead to a betterment of fatigue crack growth and fracture toughness are discussed in context of the present experimental results.
机译:先进航空技术的飞速发展,对开发新一代飞机发动机结构材料的需求日益增长。低密度金属间化合物材料和提高的高温断裂韧性表明,有望取代广泛使用的镍基高温合金。作为有序的Ti和Al的金属间化合物,TiAl和Ti {sb3 {dollar} Al由于重量轻,强度高而成为近年来研究活跃的课题。对于在金属间化合物是候选材料的耐损伤,疲劳关键的结构应用中,了解这些金属间化合物在环境温度和高温下对准静态和循环载荷断裂的抵抗力至关重要。本文探讨了Ti-Al和Ti-Al-Nb合金的微观结构,微观结构稳定性,力学变量(如载荷比和疲劳频率)以及温度对准静态和疲劳裂纹扩展特征的影响。在受控热处理的帮助下,包含{美元}αsb2{美元}和{美元}β{美元}或{美元}αsb2{美元}和{美元}γ{美元}的双相微观结构以及主要{美元}产生了}αsb2{美元}相微结构。在从阈值到最终失效的一系列{K}值{K}范围内,可以监测疲劳裂纹的扩展特性。根据TEM观察到的裂纹尖端损伤,断裂表面氧化的扫描俄歇光谱和扫描电子断层扫描,检查了可控的微观结构对整体疲劳和抗断裂性能的影响。根据它们对疲劳裂纹扩展和断裂韧性的响应,检查了它们的稳定性。在本实验结果的背景下讨论了导致疲劳裂纹扩展和断裂韧性得到改善的微观结构特征。

著录项

  • 作者

    Aswath, Pranesh Belgod.;

  • 作者单位

    Brown University.;

  • 授予单位 Brown University.;
  • 学科 Engineering Materials Science.; Engineering Metallurgy.
  • 学位 Ph.D.
  • 年度 1990
  • 页码 217 p.
  • 总页数 217
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;冶金工业;
  • 关键词

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