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On the characterization of Johnson-Cook constants : numerical and experimantal study of high speed machining aerospace alloys

机译:恒约翰逊 - 库克的特征:高速加工航空航天合金

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摘要

The aerospace industry would eventually replace chemical machining by mechanical machining which is more accurate, more predictable and more ecological. In fact, the discharges in the case of chemical machining contain especially carbon dioxide and solvents that are difficult to degrade in groundwater. The mechanical machining also avoids an important quantity of hazardous substances and provides better chips recycling. However, the control of mechanical machined parts quality goes through the prediction and the optimization of the metal cutting processes. The most attractive computational tool to predict and optimize metal cutting processes is the finite element modeling (FEM). The success and the reliability of any FEM depend strongly on the constitutive laws which describe the thermo-mechanical behavior of the machined materials. The most commonly used one is that of Johnson and Cook (JC) which combines the effect of strains, strain rates, and temperatures. The determination of the material constants of JC under high strains, strain rates, and temperatures during machining conditions has long been a major challenge but a necessity for those who apply finite element modeling techniques in machining processes at the chip formation scale.ududThis study aims at treating this subject in order to better understand the effect of the JC constitutive law on the prediction of cutting parameters (cutting forces, residual stresses, etc.) for aluminum alloys. In addition, in order to meet the interests of aerospace industry, three aluminum alloys (Al2024-T3, Al6061-T6 and Al7075-T6) commonly used in aircraft applications have been selected.ududThis research work is divided into three consecutive steps.ududFirstly, a new approach to identify the material constants of JC for metal cutting is proposed. The approach is based on the inverse method (orthogonal machining tests) and the response surface methodology which allows generating a large number of cutting conditions within fixed ranges of cutting speed, feed rate, and rake angle. Based on this approach, the sensitivity of the material constants of JC to the rake angle for the three alloys was analysed. It was found that, for these three alloys, one set of the material constants obtained from the proposed approach predicts more accurate values of flow stresses as compared to those reported in the literature. Moreover, a 2D FEM investigation of the orthogonal cutting also showed a good agreement between the predicted cutting parameters (cutting forces and chip thickness) and experimental ones when using the material constants obtained by the proposed approach.ududSecondly, a specific focus was put on the influence of the rake angle on the material constants of JC and hence on the predicted cutting parameters (cutting forces, chip morphology, and tool-chip contact length). To achieve this goal, different sets of JC constants obtained at different rake angles (-8°, -5°, 0°, +5°, and +8°) were used in conjunction with a 2D finite element model to simulate the machining behavior of Al2024-T3 alloy. It was found that the material constants set obtained with 0° rake angle gives overall more accurate predictions of the cutting parameters as compared to other studied sets.ududFinally, the last step of this study is devoted to the prediction of induced residual stresses within the machined workpiece (Al2024-T3) and the temperature of the cutting tool(uncoated carbide). Three sets of JC based on the results obtained from the previous step with rake angles of -8°, 0°, and +8° were considered. Two finite element models were used; a 2D thermo-mechanical simulation to simulate chip formation and a 3D pure thermal analysis to obtain the temperature distribution. The results show that a better prediction of the residual stresses is obtained with JC at 0° while the other sets of JC at -8° and +8° tend to overestimate or underestimate the measured residual stresses, respectively. As far as the temperature of the cutting tool is concerned, the average values of the predicted températures of the cutting tool for each studied set of JC was considered in order to evaluate the best prediction. Based on these average values, the effect of the three sets of JC was not significant since the difference between the measured temperatures and the predicted average ones are less than 5.5% with the three cutting conditions.
机译:航空航天工业最终将用更精确,更可预测且更生态的机械加工代替化学加工。实际上,在化学机械加工的情况下,排放物中尤其含有二氧化碳和难以在地下水中降解的溶剂。机械加工还可避免大量有害物质,并提供更好的切屑回收利用。但是,机械加工零件质量的控制要经过金属切削过程的预测和优化。预测和优化金属切削过程的最有吸引力的计算工具是有限元建模(FEM)。任何FEM的成功与可靠性在很大程度上取决于构成定律,该定律描述了加工材料的热机械行为。最常用的一种是Johnson and Cook(JC)的产品,它结合了应变,应变速率和温度的影响。长期以来,在加工条件下确定高应变,应变速率和温度下的JC材料常数一直是一项重大挑战,但对于那些在切屑形成规模上将有限元建模技术应用于加工过程的人来说,这是必需的。本研究旨在处理该主题,以便更好地理解JC本构定律对铝合金切削参数(切削力,残余应力等)的预测效果。此外,为了满足航空航天业的利益,已选择了飞机应用中常用的三种铝合金(Al2024-T3,Al6061-T6和Al7075-T6)。 ud ud这项研究工作分为三个连续步骤。 ud ud首先,提出了一种新的方法来确定用于金属切削的JC的材料常数。该方法基于逆方法(正交加工测试)和响应面方法,该方法允许在切削速度,进给速度和前角的固定范围内生成大量切削条件。基于这种方法,分析了三种合金的JC材料常数对前角的敏感性。已发现,对于这三种合金,与文献中报道的相比,从所提出的方法中获得的一组材料常数可预测出更精确的流变应力值。此外,当使用通过该方法获得的材料常数时,正交切削的二维有限元分析也显示了预测的切削参数(切削力和切屑厚度)与实验参数之间的良好一致性。 ud ud其次,一个特定的重点是前角对JC的材料常数的影响,因此对预测的切削参数(切削力,切屑形态和刀具与切屑的接触长度)也有影响。为了实现此目标,将在不同前角(-8°,-5°,0°,+ 5°和+ 8°)下获得的不同JC常数集与2D有限元模型结合使用来模拟加工Al2024-T3合金的行为已经发现,与其他研究组相比,以0°前角获得的材料常数组可以总体上更准确地预测切削参数。 ud ud最后,本研究的最后一步专门用于预测残余应力。在加工的工件(Al2024-T3)和切削刀具的温度(无涂层硬质合金)内。基于前一步骤获得的三组JC,前角为-8°,0°和+ 8°。使用了两个有限元模型。 2D热机械模拟可模拟切屑的形成,而3D纯热分析可获取温度分布。结果表明,在0°时,JC可以更好地预测残余应力,而在-8°和+ 8°时,其他JC集分别倾向于高估或低估了测得的残余应力。就切削工具的温度而言,考虑每个JC研究集的切削工具预测温度的平均值,以便评估最佳预测。基于这些平均值,由于在三种切割条件下测得的温度与预测的平均值之间的差异小于5.5%,因此三套JC的效果并不显着。

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    Daoud Monzer;

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  • 年度 2016
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