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首页> 外文期刊>Journal of Materials Science & Technology >Experimental Investigation and Numerical Simulation of the Grain Size Evolution during Isothermal Forging of a TC6 Alloy
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Experimental Investigation and Numerical Simulation of the Grain Size Evolution during Isothermal Forging of a TC6 Alloy

机译:TC6合金等温锻造过程中晶粒尺寸演变的实验研究与数值模拟

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Hot compression was conducted at a Thermecmaster-Z simulator, at deformation temperatures of 800~1040 deg C, with strain rates of 0.001~50 s~(-1) and height reduction of 50 percent. Grain size of the prior a phase was measured with a Leica LABOR-LUX12MFS/ST microscope to which QUANTIMET 500 software for image analysis for quantitative metallography was linked. According to the present experimental data, a constitutive relationship for a TC6 alloy and a model for grain size of the prior a phase were established based on the Arrhenius' equation and the Yada's equation, respectively. By finite element (FE) simulation, deformation distribution was determined for isothermal forging of a TC6 aerofoil blade at temperatures of 860~940 deg C and hammer velocities of 9~3000.0 mm/min. Meanwhile, the grain size of the prior a phase is simulated during isothermal forging of the TC6 aerofoil blade, by combining FE outputs with the present grain size model. The present results illustrate the grain size and its distribution in the prior a phase during the isothermal forging of the TC6 aerofoil blade. The simulated results show that the height reduction, deformation temperature, and hammer velocity have significant effects on distribution of the equivalent strain and the grain size of the prior a phase.
机译:在Thermecmaster-Z仿真器上进行热压缩,变形温度为800〜1040℃,应变速率为0.001〜50 s〜(-1),高度降低50%。前一相的晶粒尺寸使用Leica LABOR-LUX12MFS / ST显微镜测量,该显微镜连接了用于定量金相图像分析的QUANTIMET 500软件。根据目前的实验数据,分别基于Arrhenius方程和Yada方程建立了TC6合金的本构关系和先有相的晶粒尺寸模型。通过有限元(FE)模拟,确定了TC6翼型叶片在860〜940摄氏度的温度和9〜3000.0 mm / min的锤击速度下的等温锻造的变形分布。同时,通过将有限元输出与当前晶粒尺寸模型相结合,在TC6翼型叶片的等温锻造过程中模拟了前一相的晶粒尺寸。本结果说明了TC6翼型叶片的等温锻造过程中前一阶段的晶粒尺寸及其分布。模拟结果表明,高度降低,变形温度和锤击速度对前一相的等效应变的分布和晶粒尺寸具有显着影响。

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