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首页> 外文期刊>Silicon >Microstructure and Wear Behavior of Single layer (CrN) and Multilayered (SiN/CrN) Coatings on Particulate Filled Aluminum Alloy Composites
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Microstructure and Wear Behavior of Single layer (CrN) and Multilayered (SiN/CrN) Coatings on Particulate Filled Aluminum Alloy Composites

机译:颗粒填充铝合金复合材料上单层(CrN)和多层(SiN / CrN)涂层的组织和磨损行为

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This article presents the slurry erosive wear behavior of single and multilayer coatings on granite powder reinforced aluminum alloy composites for hydro-turbine blade material. The composites were fabricated by stir casting technique with different weight fraction (0, 2, 4, 6wt.%) of granite powder in 1050 aluminum alloy. In this study, the slurry jet erosive performance of uncoated, single layer and multilayer coating granite powder filled alloy composites in a slurry jet wear test was conducted for four different operating parameters such as filler content (0-6wt.%), impact velocity (10-25 m/s), impingement angle (30-75 (0)) and erodent discharge (160-280 gm), respectively. The slurry erosion rate was a maximum at 0wt.% granite powder reinforcement in uncoated, single layer and multilayer coating samples such as: 0.0203 gm/kg, 0.00981 gm/kg and 0.00756 gm/kg, respectively at impact velocity of 25 m/sec. Taguchi's orthogonal array (L (16)) was applied to study the experimental results of the uncoated and coated alloy composites. A correlation was derived from the results of the Taguchi experimental design and a proposed predictive equation for estimation of slurry erosion rate of these composites. Atomic force microscopy (AFM) and scanning electron microscopy (SEM) were conducted to analyze the topography of the eroded surface of uncoated and coated granite powder reinforced aluminum alloy composites.
机译:本文介绍了用于水轮机叶片材料的花岗岩粉末增强铝合金复合材料上单层和多层涂层的浆液腐蚀磨损行为。通过搅拌铸造技术用1050铝合金中不同重量分数(0、2、4、6wt。%)的花岗岩粉末制造复合材料。在这项研究中,针对四种不同的操作参数(如填料含量(0-6wt。%),冲击速度(%),对未涂覆的,单层和多层涂覆的花岗岩粉末填充的合金复合材料的浆料喷射侵蚀性能进行了浆料喷射磨损测试。 10-25 m / s),撞击角(30-75(0))和腐蚀放电(160-280 gm)。在未涂覆,单层和多层涂层的样品中,在0wt。%的花岗岩粉末增强下,浆液侵蚀速率最大,例如在25 m / sec的冲击速度下分别为0.0203 gm / kg,0.00981 gm / kg和0.00756 gm / kg 。 Taguchi的正交阵列(L(16))用于研究未涂层和涂层合金复合材料的实验结果。从田口实验设计的结果和提出的用于估计这些复合材料的浆液侵蚀速率的预测方程式可以得出相关性。进行了原子力显微镜(AFM)和扫描电子显微镜(SEM)分析未涂覆和涂覆的花岗岩粉末增强铝合金复合材料的腐蚀表面形貌。

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