开发 A A7075-B4C 复合材料-钢界面磨损系数公式

Venkatrami Reddy Veduru, R. R, Kanulla Karthik, P. Sasirekha
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摘要

在这项研究中,我们尝试为特定磨损状态建立一个磨损方程,该磨损方程随温度、滑动速度、施加载荷和滑动距离的不同而不同。实验运行采用 L25 Taguchi 正交阵列设计,并使用扫描电子显微镜确认了强化剂的均匀分散。增强体的存在阻碍了位错运动,从而提高了复合材料的硬度,而温度的升高则由于皮尔斯应力的降低而导致硬度下降。由于形成了机械混合层(MML),磨损率随着 B4C 颗粒体积分数的增加而降低,直到 7.5%,超过这一比例后,MML 破裂,由于直接金属接触,磨损率从轻微变为严重。在 50°C 时,磨损模式为磨蚀和分层;在 150°C 时,磨损模式为磨蚀塑性变形;在 250°C 时,磨损模式为材料塑性流动。在磨损表面形态上观察到的明显特征有沟槽、微坑、微裂纹、犁沟和分解材料。通过将强化效应、特定磨损机制、温度相关因素和功能参数纳入其中,建立了修正的磨损方程。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of a Wear Coefficient Equation for the A A7075-B4C Composite – Steel Interface
In this research, an attempt was made to develop a wear equation for specific wear regimes that differs with temperature, sliding velocity, applied load, and sliding distance. The experimental runs were designed with the L25 Taguchi orthogonal array, and the uniform dispersion of reinforcement was confirmed using a scanning electron microscope. The presence of reinforcement hinders dislocation movement led to an augmentation in the composites' hardness, while an elevation in temperature resulted in a decline in hardness due to the reduction of Pierls stresses. Owing to the formation of a Mechanical Mixed Layer (MML), the wear rate decreases with addition of volume fraction of B4C particles until 7.5%, beyond this MML break down and wear rate transit from mild to severe due to the direct metal contact. At 50°C, the wear mode was abrasive and delamination; at 150°C, it was abrasive plastic deformation; and at 250°C, it was plastic flow of materials. Grooves, micro pits, micro cracks, ploughing and resolidified material were the distinct feature observed on the worn surface morphology. The modified wear equation was developed by incorporating reinforcement effect, specific wear regimes, temperature-dependent factors, and functional parameters.
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