Wear Behaviour of Aluminium Alloy 8011 with 4% Fly Ash Composites by Using Sensitivity Analysis

S. Magibalan
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引用次数: 2

Abstract

The current research work is focused on fabrication of Aluminium Alloy 8011 with 4% fly ash composite (AA8011-4% FA) by using the stir casting method. Wear behaviour and description of the composite are evaluated in different process parameters by using a pin-on-disc at room temperature. Fly ash (FA) in the range of (4 wt. %, average micron size 10 – 30 μ m) is included into the matrix, and its sensitivity analysis is investigated. Three level of Central Composite Design model is developed by using Response Surface Methodology equation with different process parameters via load, time and sliding velocity are separate in the range of (5 – 15 N), (5 – 15 min) and (1.5 – 4.5 m/s) respectively. The surface plot shows that wear rate increases with increasing load, time and sliding velocity. A sensitivity analysis is also carried out and compared with the relative impact of input parameters on wear behaviour in order to verify the measurement errors on the values of the uncertainty in estimated parameters of three inputs such as normal load, time and sliding velocity on wear rate (WR) and coefficient of friction (COF). The result shows that normal load is more sensitive than the other parameters. The variation of load causes more changes in wear rate.
4%粉煤灰复合材料对8011铝合金磨损性能的敏感性分析
采用搅拌铸造法制备了4%粉煤灰复合材料(AA8011-4% FA)铝合金8011。在不同的工艺参数下,通过在室温下使用销盘来评估复合材料的磨损行为和描述。在基质中加入4 wt. %的粉煤灰(FA),平均粒径为10 ~ 30 μ m,并对其进行敏感性分析。利用响应面法方程建立了三个层次的中央复合设计模型,不同的工艺参数通过载荷、时间和滑动速度分别在(5 ~ 15 N)、(5 ~ 15 min)和(1.5 ~ 4.5 m/s)范围内分离。磨损率随载荷、时间和滑动速度的增加而增加。为了验证法向载荷、时间和滑动速度三种输入参数的估计参数的不确定度值对磨损率(WR)和摩擦系数(COF)的测量误差,还进行了灵敏度分析,并与输入参数对磨损行为的相对影响进行了比较。结果表明,正常负载比其他参数更敏感。载荷的变化引起磨损率的较大变化。
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