金属中任意尺寸和位置的内部缺陷的增材制造技术及疲劳性能评价

Kazuyuki Morishita, Taichi Yamaguchi, K. Wada, J. Yamabe
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引用次数: 0

摘要

机械部件的失效通常是由金属材料的微小缺陷引起的金属疲劳引起的。因此,精确地捕捉含有小缺陷的材料的疲劳特性是很重要的。对钻孔引入人工表面缺陷的材料进行了疲劳试验。利用所得数据,提出了基于√面积参数模型的材料疲劳极限预测方程,并验证了其对各种材料的有效性。然而,对于含有内部缺陷导致失效的增材制造(AM)材料,控制断裂起源处缺陷的尺寸是非常困难的。因此,与其他材料由于表面缺陷而失效相比,无法验证增材制造材料的√面积参数模型的预测能力。在这种情况下,开发一种在任意位置有意引入任意尺寸的内部缺陷的技术,可以提供有助于预测增材制造材料疲劳极限的见解。本研究旨在通过增材制造在任意位置引入任意尺寸的内部缺陷,建立一种定量评估内部缺陷对增材制造材料疲劳性能影响的技术。制备了不同缺陷尺寸和位置的试样。在疲劳试验之前,通过x射线计算机断层扫描(CT)对缺陷的尺寸和位置进行了非破坏性测量。疲劳试验在室温空气中进行。除靠近表面缺陷的试样外,所有试样均因故意引入内部缺陷而失效,随着缺陷尺寸的增大,疲劳寿命逐渐缩短。在这种情况下,疲劳裂纹很容易到达表面;因此,推测其疲劳寿命比具有相同缺陷尺寸的试样短。此外,从断口表面扫描电镜测定的缺陷尺寸与x射线CT测定的几乎一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Technique for Introducing Internal Defects with Arbitrary Sizes and Locations in Metals via Additive Manufacturing and Evaluation of Fatigue Properties
Mechanical component failure is usually caused by metal fatigue originating from small defects in metallic materials. Thus, it is important to precisely capture the fatigue properties of materials containing small defects. Fatigue tests of materials with artificial surface defects introduced by drilling have been conducted. Using the resulting data, an equation for predicting the material fatigue limit has been proposed on the basis of the √area parameter model, and its effectiveness has been confirmed for various materials. However, for additive manufactured (AM) materials that contain internal defects resulting in failure, controlling the size of the defect where the fracture originates is extremely difficult. Therefore, verification of the predictive ability of the √area parameter model for AM materials is impossible, in contrast with other materials that fail because of surface defects. In this context, developing a technique to intentionally introduce internal defects with arbitrary sizes at arbitrary locations can provide insights that help predict the fatigue limit of AM materials. This study aimed to establish a technology for quantitatively evaluating the effect of internal defects on the fatigue properties of AM materials by introducing internal defects with arbitrary sizes at arbitrary locations via AM. Specimens with different defect sizes and locations were prepared. Prior to the fatigue tests, the defect sizes and locations were measured non-destructively via X-ray computed tomography (CT). The fatigue tests were conducted in air at room temperature. All the specimens failed because of the intentionally introduced internal defects, and the fatigue lives became shorter with increasing defect sizes, except for the specimens with defects adjacent to the surface. In those cases, fatigue cracks easily reached the surface; therefore, the fatigue lives were speculated to be shorter than those of the specimens with the same defect sizes. Moreover, the defect sizes determined from the fracture surfaces by scanning electron microscopy were nearly consistent with those determined by X-ray CT.
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