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Experiments and numerical simulations for the fatigue behavior of a novel TA2-TA15 titanium alloy fabricated by laser melting deposition

机译:激光熔融沉积制备新型TA2-TA15钛合金疲劳行为的实验和数值模拟

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摘要

In this paper, experiments and numerical simulations are conducted to investigate the fatigue behavior of a novel TA2-TA15 titanium alloy fabricated by the laser melting deposition (LMD) manufacturing process. First, the uniaxial tensile and fatigue experiments of the LMD TA2-TA15 specimens are carried out to acquire the basic static mechanical and fatigue properties, and the experimental results show that the values of Young's module, yield stress, ultimate stress and fatigue limit of the LMD TA2-TA15 material are between that of the TA2 and TA15 materials. Moreover, the dispersion of data in the experimental fatigue lives are observed, and then the fracture surfaces of the LMD TA2-TA15 specimens are tested by the scanning electron microscope (SEM), revealing that the dispersion is primarily caused by the multiple sources of cracks and the manufacturing defects inside the specimens. After that, several recommendations are provided for the better applications of different titanium alloys based on the engineering requirements and economy consideration. At last, the fatigue lives are numerically predicted for the LMD TA2-TA15 titanium alloy, which are compared with the experimental data. The further investigations of the predicted fatigue damage behavior indicate that the damage variable and the damage evolution rate increase fast with the increase of the number of cycles, resulting in the rapid decrease of the Young's modulus and the von Mises stress, when the loading cycles reach to 90% of the fatigue life.
机译:在本文中,进行了实验和数值模拟,以研究通过激光熔融沉积(LMD)制造工艺制造的新型TA2-TA15钛合金的疲劳行为。首先,对LMD TA2-TA15试样进行了单轴拉伸和疲劳试验,以获取基本的静态力学和疲劳性能,并且实验结果表明,杨氏模量,屈服应力,极限应力和疲劳极限值LMD TA2-TA15材料介于TA2和TA15材料之间。此外,观察了实验疲劳寿命中数据的分散,然后通过扫描电子显微镜(SEM)测试了LMD TA2-TA15标本的断裂表面,发现分散主要是由多种裂纹源引起的以及样品内部的制造缺陷。之后,根据工程要求和经济考虑,提出了一些建议,以更好地应用不同的钛合金。最后,对LMD TA2-TA15钛合金的疲劳寿命进行了数值预测,并与实验数据进行了比较。对预测的疲劳损伤行为的进一步研究表明,随着载荷循环次数的增加,损伤变量和损伤演化速率迅速增加,导致当载荷周期达到一定时,杨氏模量和冯·米塞斯应力迅速下降。达到90%的疲劳寿命。

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