Ab'/> Low cycle fatigue, creep and creep-fatigue interaction behavior of a TiAl alloy at high temperatures
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Low cycle fatigue, creep and creep-fatigue interaction behavior of a TiAl alloy at high temperatures

机译:高温下的Tial合金的低循环疲劳,蠕变和蠕变 - 疲劳相互作用行为

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摘要

AbstractThe creep-fatigue interaction (CFI) tests of a TiAl alloy were carried out at 750°C and 800°C in air to investigate the effect of dwell time on fatigue life. The low cycle fatigue (LCF) and creep tests were also conducted for comparison. The life to failure decreased with increasing dwell time and decreased with increasing minimum strain rate. Two life models based on dwell time and minimum strain rate were proposed to predict LCF, creep and CFI life, and the predicted life of both life models agrees very well with the tested life of the alloy at high temperatures.Graphical abstract(a) Evolution of the mean strain with the cyclic time increasing under different dwell times at 750°C; (b) Evolution of the mean strain with the cyclic time increasing under different dwell times at 800°C.(c) Normalized time to failure (Tf/Tf?LCF) vs. effective dwell time (△t/tp) at 750°C and 800°C; (d) Comparison between predicted life by Model I and tested life.(e) Normalized time to failure (Tf/Tf-creep) vs. normalized minimum strain rate (ε?min/ε?min,creep) at 750°C and 800°C; (f) Comparison between predicted life by Model II and tested life.Display Omitted]]>
机译:<![cdata [ 抽象 Tial合金的蠕变 - 疲劳相互作用(CFI)在750°C和800°进行Tial合金的测试C在空气中调查停留时间对疲劳生活的影响。还进行了低循环疲劳(LCF)和蠕变试验进行比较。随着停留时间的增加而失效的生命减少,随着最小应变率的增加而降低。提出了基于停留时间和最小应变速率的两种寿命模型,以预测LCF,蠕变和CFI寿命,并且寿命模型的预测寿命与高温下合金的测试寿命非常好。 图形抽象 (a)循环平均应变的演变在750°C下不同停留时间增加时间; (b)平均菌株的循环时间在800°C的不同停留时间下增加。 (c)归一化的失败时间( t f / t f lcf )与750°C和800°C的有效停留时间(△T/ T P ); (d)通过模型I和测试生命之间的预测寿命比较。 (e)归一化的失败时间(t F / T F-CREEP )与归一化最小应变率( ε min < / mml:msub> / ε < / MML:MIVER> MIN CREEP ),750°C和800°C; (f)模型II和测试生命之间的预测寿命比较。 显示省略 ]]>

著录项

  • 来源
    《Scripta materialia》 |2018年第2018期|共4页
  • 作者单位

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation Aviation Key Laboratory of Science and Technology on Aeronautical Materials Testing and Evaluation Science and Technology on Advanced High Temperature Structural Materials Laborator;

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation Aviation Key Laboratory of Science and Technology on Aeronautical Materials Testing and Evaluation Science and Technology on Advanced High Temperature Structural Materials Laborator;

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation Aviation Key Laboratory of Science and Technology on Aeronautical Materials Testing and Evaluation Science and Technology on Advanced High Temperature Structural Materials Laborator;

    School of Materials Science and Engineering Harbin Institute of Technology;

    School of Materials Science and Engineering Harbin Institute of Technology;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 冶金工业;
  • 关键词

    TiAl alloy; Low cycle fatigue (LCF); Creep-fatigue interaction (CFI); Dwell time; Life prediction;

    机译:Tial合金;低循环疲劳(LCF);蠕变 - 疲劳相互作用(CFI);停留时间;生活预测;

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