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Material Parameter Identification and Response Prediction of Shearing Process for Flying Shear Machine Based on Model Validation

机译:基于模型验证的飞行剪切机剪切过程的材料参数识别与响应预测

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This paper studies on the simulation of a certain type of flying shear machine's the shearing process. In the finite element simulation, chip formation and cutting ability is not only affected by the high temperature of bar itself and impact velocity of cutter, but also affected by the material itself stress-strain curve under different strain rate and fracture model. Even if the same temperature and impact velocity for high temperature bar, due to the uncertainty of different parameters under different strain rate stress-strain curves, different fracture model, different critical damage factor, the maximum shear force and shear punch depth are not the same. Therefore, in order to obtain a more accurate finite element model and response prediction, it is necessary to identify the uncertainties of the parameters for the material constitutive model and fracture criterion. According to the principle of equivalent energy, the research group designed a kind of falling hammer punching test rig, and the high temperature (700-900°C) bars of 1Cr18Ni9Ti, Φ10 and Φ20 bars experiments were conducted with multiple groups of shock shear tests. With the aid of the data acquisition instrument, the acceleration parameter of impact shearing process is collected. At the same time, for punching and shearing test numerical simulation was conducted based on nonlinear metal forming finite element analysis. By Φ20 bars punching test results and simulation results and model updating method, the parameter identification method about stress-strain curve under different strain rate and critical damage factor in material fracture criterion of high temperature bar in punching process is studied. And then the prediction for shearing process of Φ10 was verified by comparing with the test result. After obtaining reasonable and accurate material parameters, for the real flying shear machine, the numerical simulation of Φ160 high temperature bar is carried out under the equivalent impact mass and shear speed. The parameter identification method has practical significance to predict and optimize the shearing performance of different types of flying shear for shearing section steel with different materials and different sections. The results show that: the validation method based on the combination of test data and model updating is effective, which can be applied to discriminate and predict material parameters of similar structures of shearing high temperature bar in engineering.
机译:本文研究了某种类型的飞剪机器剪切过程的仿真研究。在有限元模拟中,芯片形成和切割能力不仅受到杆本身的高温和切割器的冲击速度影响,而且受到不同应变率和裂缝模型的材料本身应力 - 应变曲线的影响。即使高温棒的温度和冲击速度相同,由于不同应变率应力曲线下不同参数的不确定性,不同的断裂模型,不同的临界损伤因子,最大剪切力和剪切冲击深度不一样。因此,为了获得更准确的有限元模型和响应预测,有必要识别材料本构模型和裂缝标准的参数的不确定性。根据等效能量的原理,研究组设计了一种倒下的锤式冲孔试验台,并且通过多组冲击剪切测试进行高温(700-900°C)的1Cr18Ni9Ti,φ10和φ20BAR实验。借助数据采集仪器,收集了冲击剪切过程的加速度参数。同时,基于非线性金属形成有限元分析,对冲压和剪切测试进行数值模拟。通过φ20棒冲压测试结果和模拟结果和模型更新方法,研究了在冲压过程中不同应变速率下的应力 - 应变曲线的参数识别方法,以及冲压过程中的高温棒的材料断裂标准中的临界损伤因子。然后通过与测试结果进行比较来验证φ10的剪切过程的预测。获得合理和准确的材料参数后,对于实际飞行剪切机,φ160高温棒的数值模拟在等效的冲击质量和剪切速度下进行。参数识别方法具有预测和优化不同类型的剪切段钢的剪切性能,具有不同的材料和不同的部分的实际意义。结果表明:基于测试数据和模型更新组合的验证方法是有效的,可以应用于在工程中剪切高温棒类似结构的区分和预测材料参数。

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