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Prediction of short fatigue crack growth of Ti-6Al-4V

机译:Ti-6Al-4V短时疲劳裂纹扩展的预测

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摘要

It is observed that the short fatigue cracks grow faster than long fatigue cracks at the same nominal driving force and even grow at stress intensity factor range below the threshold value for long cracks in titanium alloy materials. The anomalous behaviours of short cracks have a great influence on the accurate fatigue life prediction of submersible pressure hulls. Based on the unified fatigue life prediction method developed in the authors' group, a modified model for short crack propagation is proposed in this paper. The elastic-plastic behaviour of short cracks in the vicinity of crack tips is considered in the modified model. The model shows that the rate of crack propagation for very short cracks is determined by the range of cyclic stress rather than the range of the stress intensity factor controlling the long crack propagation and the threshold stress intensity factor range of short fatigue cracks is a function of crack length. The proposed model is used to calculate short crack propagation rate of different titanium alloys. The short crack propagation rates of Ti-6Al-4V and its corresponding fatigue lives are predicted under different stress ratios and different stress levels. The model is validated by comparing model prediction results with the experimental data.
机译:可以看出,在相同的标称驱动力下,短疲劳裂纹的生长快于长疲劳裂纹,甚至在低于钛合金材料中长裂纹阈值的应力强度因子范围内生长。短裂纹的异常行为对潜水耐压船体的准确疲劳寿命预测有很大的影响。基于作者小组开发的统一疲劳寿命预测方法,本文提出了一种改进的短裂纹​​扩展模型。在改进模型中考虑了裂纹尖端附近短裂纹的弹塑性行为。该模型表明,非常短的裂纹的裂纹扩展速率是由循环应力的范围决定的,而不是由控制长裂纹扩展的应力强度因子的范围决定的,而短疲劳裂纹的阈值应力强度因子的范围是函数的函数。裂纹长度。该模型用于计算不同钛合金的短裂纹扩展速率。在不同的应力比和不同的应力水平下,预测了Ti-6Al-4V的短裂纹扩展速率及其相应的疲劳寿命。通过将模型预测结果与实验数据进行比较来验证模型。

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  • 作者单位

    School of Naval Architecture, Ocean and Civil Engineering, Shanghai Jiao Tong University Shanghai 200030, China,School of Naval Architecture and Ocean Engineering, Jiangsu University of Science and Technology Zhenjiang 212003, China;

    Hadal Science and Technology Research Center, Shanghai Ocean University Shanghai 201306, China;

    Hadal Science and Technology Research Center, Shanghai Ocean University Shanghai 201306, China,Nonlinear Analysis and Applied Mathematics (NAAM) Research Group, Faculty of Science, King Abdulaziz University Jeddah 21589, Saudi Arabia;

    Nonlinear Analysis and Applied Mathematics (NAAM) Research Group, Faculty of Science, King Abdulaziz University Jeddah 21589, Saudi Arabia,Department of Mathematics, Quaid-i-Azam University Islamabad 45320, Pakistan;

    Nonlinear Analysis and Applied Mathematics (NAAM) Research Group, Faculty of Science, King Abdulaziz University Jeddah 21589, Saudi Arabia;

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  • 原文格式 PDF
  • 正文语种 eng
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  • 关键词

    crack propagation threshold; fatigue crack propagation rate; short fatigue cracks; titanium alloy; unified fatigue life prediction method;

    机译:裂纹扩展阈值疲劳裂纹扩展率;疲劳裂纹短;钛合金统一疲劳寿命预测方法;

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