基于有限元模拟的多参数优化提高涂层耐蚀性

Fang Li, Shunsen Wang, Liuxi Cai, Z. Feng
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引用次数: 0

摘要

采用有限元法研究了4种典型耐蚀涂层(Fe2B、CrN、Cr3C2-NiCr和Al2O3-13%TiO2)在汽轮机叶片表面应力S11 (x轴径向应力分量)的应力峰值。分析了冲击速度、涂层厚度、杨氏模量和泊松比等4个参数对应力S11应力峰值的影响。结果表明:随着冲击速度的增加,应力S11的拉应力峰值和压应力峰值的位置远离冲击中心点;当涂层厚度大于等于10μm时,在不同冲击速度下,四个涂层表面应力S11的拉应力峰值大小不随涂层厚度的变化而变化。当涂层厚度大于等于2μm时,随着杨氏模量的增加,4种涂层的应力S11拉应力峰值大小均呈现先增大后减小的趋势。同时,泊松比越大,应力S11的拉应力峰值越小。优化后,当涂层厚度为2μm、泊松比为0.35、杨氏模量为800 GPa时,相同冲击条件下,Fe2B涂层的抗冲蚀性能最强,Cr3C2-NiCr、CrN次之,Al2O3-13%TiO2涂层的抗冲蚀性能最差。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Multi-Parameter Optimization to Improve the Erosion Resistance of Coating by FE Simulation
Finite element method (FEM) was used to study the stress peak of stress S11 (Radial stress component in X-axis) on the steam turbine blade surface of four typical erosion-resistant coatings (Fe2B, CrN, Cr3C2-NiCr and Al2O3-13%TiO2). The effect of four parameters, such as impact velocity, coating thickness, Young’s modulus and Poisson’s ratio on the stress peak of stress S11 were analyzed. Results show that: the position of tensile stress peak and compressive stress peak of stress S11 are far away from the impact center point with the increase of impact velocity. When coating thickness is equal to or greater than 10μm, the magnitude of tensile stress peak of stress S11 on the four coating surfaces does not change with the coating thickness at different impact velocities. When coating thickness is equal to or greater than 2μm, the magnitude of tensile stress peak of stress S11 of four coatings show a trend of increasing first and then decreasing with the increase of Young’s modulus. Meanwhile, the larger the Poisson’s ratio, the smaller the tensile stress peak of stress S11. After optimization, When coating thickness is 2μm, Poisson’s ratio is 0.35 and Young’s modulus is 800 GPa, the Fe2B coating has the strongest erosion resistance under the same impact conditions, followed by Cr3C2-NiCr, CrN, and the Al2O3-13%TiO2 coating, Al2O3-13%TiO2 coating has the worst erosion resistance.
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