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基于摩擦修正的TC6钛合金低应变速率大变形本构模型建立 被引量:1

Low Strain Rate and Large Deformation Constitutive Model of TC6 Titanium Alloy Based on Friction Correction
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摘要 采用Thermecmastor-Z100kn热模拟试验机对TC6钛合金进行了低应变速率大变形热压缩试验,获得了变形温度范围为900~945℃、应变速率范围为0.0001~0.1 s^(-1)、变形程度为70%时的真应力-真应变曲线。分别使用传统摩擦修正模型与改进摩擦修正模型对真应力-真应变曲线进行修正,并建立了基于摩擦修正的应变补偿型Arrhenius模型。结果表明:改进摩擦修正模型能更好地表征材料在大变形状态下的真应力-真应变动态响应。经摩擦模型修正的应变补偿型Arrhenius模型相线性相关度较高,平均绝对误差较小,预测值精度较高。 The thermal compression test of TC6 titanium alloy under low strain rate and large deformation was carried out by Thermecmastor-Z100kn thermal simulation machine.The true stress-strain curves were obtained when the deformation temperature was 900-945℃,the strain rate was 0.0001-0.1 s^(-1) and the deformation degree was 70%.The traditional friction correction model and the improved friction correction model were used to correct the true stress-strain curve,and the strain-compensated Arrhenius model based on the friction correction was established.The results show that the modified friction correction model can better characterize the true stress-strain dynamic response of materials under large deformation.The strain-compensated Arrhenius model modified by friction correction has higher linear correlation,smaller mean absolute error and higher prediction accuracy.
作者 朱琳 徐勇 胡生双 陈乐平 辛周媛 Zhu Lin;Xu Yong;Hu Shengshuang;Chen Leping;Xin Zhouyuan(Nanchang Hangkong University,Nanchang 330063,China;AVIC Xi’an Aircraft Industry Group Company Ltd,Xi’an 710089,China)
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2023年第5期1819-1825,共7页 Rare Metal Materials and Engineering
基金 航空科学基金(2019ZE056009) 江西省重点研发计划(20202BBEL53012)。
关键词 TC6钛合金 传统摩擦修正模型 改进摩擦修正模型 应变补偿型Arrhenius模型 TC6 titanium alloy traditional friction correction model improved friction correction model strain-compensated Arrhenius model
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