首页> 外文期刊>International Journal of Fatigue >High-cycle fatigue behavior of a laser powder bed fusion additive manufactured Ti-6Al-4V titanium: Effect of pores and tested volume size
【24h】

High-cycle fatigue behavior of a laser powder bed fusion additive manufactured Ti-6Al-4V titanium: Effect of pores and tested volume size

机译:激光粉床融合添加剂的高周疲劳行为制造Ti-6Al-4V钛:孔隙的影响和经测试的体积尺寸

获取原文
获取原文并翻译 | 示例
           

摘要

This work is focused on the effect of natural defect on the fatigue resistance of a laser powder bed fusion additively manufactured Ti-6A1-4V titanium. To reveal the fatigue strength variability and its sensitivity to the defect size, push-pull fatigue tests have been undertaken on specimens with different sizes of highly loaded volume of material. In order to easily vary the size of the highly loaded volume, specimens containing different numbers of surface hemispherical shape holes of 600 μm in diameter have been tested. This method also allowed to test small volume which triggered crack initiation from microstructural features. The fatigue damage mechanisms observed and the average natural defect size measured on the failure surfaces depend on the size of the highly stressed region. A higher fatigue strength is observed for smaller stressed volumes and defect free regions. To reduce the impact lack-of-fusion on fatigue and increase the probability of triggering crack initiation from a microstructural feature, the specimens were built in the horizontal direction. For specimens where fatigue cracks initiated at natural discontinuities, the results reported in a Kitagawa-Takahashi diagram revealed a critical defect size (area~(1/2)) in the range of 30 μm. In addition, a probabilistic approach based on the weakest link theory is proposed. The model describes a probabilistic Kitagawa-Takahashi diagram accounting for the size of both the highly stressed volume and the natural defect.
机译:这项工作侧重于自然缺陷对激光粉床融合的疲劳抗性的影响加剧制造了Ti-6a1-4V钛。为了揭示疲劳强度的变异性及其对缺陷尺寸的敏感性,已经在具有高负荷体积大小的不同尺寸的样品上进行了推拉疲劳试验。为了容易地改变高负载体积的尺寸,已经测试了含有600μm的不同表面半球形孔的样品。该方法还允许测试触发从微观结构特征的裂纹启动的小体积。观察到的疲劳损伤机制和在故障表面上测量的平均自然缺陷尺寸取决于高度应力区域的尺寸。观察到更高的疲劳强度,对于较小的压力,缺陷的自由区域。为了减少对疲劳缺乏融合的影响,提高从微观结构特征触发裂纹开始的概率,在水平方向上构建了标本。对于在天然不连续性发起的疲劳裂缝的标本中,KITAGAWA-TAKAHASHI图中报告的结果显示了临界缺陷尺寸(面积〜(1/2)),范围为30μm。此外,提出了一种基于最弱的链路理论的概率方法。该模型描述了概率KITAGAWA-TAKAHASHAHI图,其占高强调体积和自然缺陷的大小。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号