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Evaluation of notch size effect on LCF life of TA19 specimens based on the stress gradient modified critical distance method

机译:基于应力梯度修正临界距离法评估缺口尺寸对TA19试样LCF寿命的影响

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摘要

In the present study, the stress gradient modified critical distance method is proposed to predict the low-cycle fatigue lifetime of notched TA19 specimens by introducing a weight function of relative stress gradient into conventional critical distance theories. The accuracy and reliability of the proposed method were validated based on the experimental data by performing low-cycle fatigue tests on smooth bar TA19 specimens as well as geometrically similar plate specimens containing a bore hole (BHP). Predicted results demonstrate that the mean absolute errors for entire tested specimens using the stress gradient modified critical distance method on the basis of the point method and the line method are 7.49% and 7.41% respectively. Furthermore, the fatigue striation width at the fracture surface was determined by scanning electronic microscope observations to examine the stress gradient effect on the crack growth rate. Highlights 1. The effect of circular hole size on the LCF life is investigated experimentally. 2. SEM observations reveal that stress gradient inhibits the fatigue crack growth. 3. The conventional CDTs extended to the LCF regime fail to evaluate the notch size effect. 4. A novel method is proposed by combining weight function of relative stress gradient and CDTs.
机译:在本研究中,通过将相对应力梯度的权函数引入常规的临界距离理论中,提出了应力梯度修正临界距离方法来预测带槽TA19试样的低周疲劳寿命。通过对滑杆TA19试样以及包含钻孔(BHP)的几何相似板试样进行低周疲劳测试,基于实验数据验证了该方法的准确性和可靠性。预测结果表明,采用基于点法和线法的应力梯度修正临界距离法计算的整个试样的平均绝对误差分别为7.49%和7.41%。此外,通过扫描电子显微镜观察确定断裂表面的疲劳条纹宽度,以检查应力梯度对裂纹扩展速率的影响。要点1.实验研究了圆孔尺寸对LCF寿命的影响。 2. SEM观察表明应力梯度会抑制疲劳裂纹的扩展。 3.扩展到LCF机制的常规CDT无法评估陷波大小效应。 4.结合相对应力梯度和CDTs的权函数,提出了一种新的方法。

著录项

  • 来源
  • 作者

    R. Wang; H. Liu; D. Hu; D. Li; J. Mao;

  • 作者单位

    School of Energy and Power Engineering, Beihang University, Beijing 100191, China,Collaborative Innovation Center of Advanced Aero-Engine, Beijing 100191, China,Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing 100191, China;

    School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

    School of Energy and Power Engineering, Beihang University, Beijing 100191, China,Collaborative Innovation Center of Advanced Aero-Engine, Beijing 100191, China,Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing 100191, China;

    School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

    School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    low-cycle fatigue; notch size effect; relative stress gradient; theory of critical distances;

    机译:低周疲劳;切口尺寸效应;相对应力梯度临界距离理论;

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