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The low-cycle fatigue behavior of an alpha-two + beta titanium aluminide alloy.

机译:α-2+β铝化钛合金的低周疲劳行为。

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摘要

The role of microstructure in the LCF behavior of Ti-24Al-11Nb has been investigated. Four microstructures were selected in order to vary the size, relative orientation, and distribution of the two phases, as a means of varying the amount of deformation in the alpha-two grains and the ability of the beta phase to accommodate strain incompatibilities between them. Fully-reversed total-strain-controlled LCF and tensile testing were conducted at 25°C and 316°C. Deformation was studied by limited examination of the dislocations present in the material before and after testing and by analysis of the fatigue hysteresis loops to calculate dislocation friction and back stresses. Failure was studied by the use of fractography and the periodic replication of selected fatigue specimens. A comparison between the results of fatigue and tensile tests highlighted differences in the response under monotonic and cyclic loading. A comparison of the data at the two temperatures allowed the effects of moderate increases in alpha-two ductility to be examined, as it increases more rapidly with temperature than that of the beta phase. Microstructural effects were elucidated by differences in the behavior of the microstructures under all test conditions. Results indicate that the LCF behavior for all four microstructures can be adequately described by conventional empirical strain-based fatigue relations. For all microstructures, there was little or no plasticity-controlled fatigue at room temperature. With increasing temperature, plastic strain-life curves became steeper. Although all four microstructures showed fatigue hardening, the amount varied as it was related to the plastic component of the applied strain, which varied with microstructure and temperature. Fatigue and tensile failures occurred by the propagation of cracks, which nucleated at alpha-two slipband/grain boundary intersections. Microstructural effects on fatigue life were significant, when compared with the effect of temperature, and were attributable to differences in plastic strain resulting from a given applied total strain, because of differences in yield behavior and strain accommodation at grain boundaries. The alpha-two slip length and the volume fraction and distribution of the beta phase were found to be critical microstructurel features governing fatigue behavior.
机译:已经研究了微观结构在Ti-24Al-11Nb的LCF行为中的作用。选择了四个微观结构,以改变两个相的大小,相对取向和分布,作为改变α-两个晶粒中变形量和β相适应它们之间应变不相容性的能力的一种手段。在25°C和316°C下进行完全反向的总应变控制LCF和拉伸试验。通过有限地检查材料在测试前后的位错,并通过分析疲劳磁滞回线以计算位错摩擦力和背应力,来研究变形。通过使用断层照相术和选定的疲劳样本的定期复制研究了失效。疲劳试验和拉伸试验结果之间的比较突出了单调和循环载荷下响应的差异。两种温度下数据的比较允许检查α-2延性的适度增加的影响,因为它随温度的增加比β相的增加更快。通过在所有测试条件下微观结构的行为差异来阐明微观结构效应。结果表明,可以通过常规的基于经验应变的疲劳关系充分描述所有四个微观结构的LCF行为。对于所有微结构,在室温下几乎没有或没有可塑性控制的疲劳。随着温度的升高,塑性应变寿命曲线变得更加陡峭。尽管所有四个微结构都显示出疲劳硬化,但其数量却与所施加应变的塑性成分有关,并随微结构和温度而变化。疲劳和拉伸失效是由裂纹扩展引起的,该裂纹在α两个滑移带/晶粒边界相交处成核。与温度的影响相比,对疲劳寿命的微观结构影响是显着的,并且归因于屈服行为和晶界应变适应的差异,这是由于给定施加的总应变导致的塑性应变差异。发现阿尔法二滑移长度,β相的体积分数和分布是控制疲劳行为的关键微结构特征。

著录项

  • 作者

    Stevens, Katherine Anne.;

  • 作者单位

    The Ohio State University.;

  • 授予单位 The Ohio State University.;
  • 学科 Engineering Metallurgy.; Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 374 p.
  • 总页数 374
  • 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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