首页|基于本构模型的Inconel 718材料动态力学响应分析

基于本构模型的Inconel 718材料动态力学响应分析

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Inconel 718常用于航空航天、汽车以及医疗设备领域,其高强度和低导热性造成大切削力和高切削温度,是一种典型的难加工材料.本文通过分离式霍普金森压杆试验得到了常温下Inconel 718 的真实应力-应变曲线,通过高温硬度试验得到了该材料在不同温度下的热软化率.利用激光热导试验获取不同温度下Inconel 718 的比热容和热导率,结合真实应力-应变曲线计算不同应变下的实际变形温度.利用热软化率将变温状态下的真实应力-应变曲线修正为等温状态下的应力-应变曲线,实现了应变和温度的解耦.基于Johnson-Cook和Power-Law本构模型对上述试验结果进行了拟合,结果表明,在低应变率下Power-Low本构模型的拟合精度更高,而在高应变率下Johnson-Cook本构模型的拟合精度更高.最后通过有限元仿真探究了应变、应变率、温度单独作用下,Inconel 718材料力学性能的响应机制,发现应变对应力的影响最大,温度次之,应变率对应力基本没有影响.
Dynamic Mechanical Response Analysis of Inconel 718 Based on Constitutive Model
Inconel 718 is commonly used in aerospace,automotive and medical equipment,but it is a typical difficult-to-machine material due to its high strength and low thermal conductivity,resulting in large cutting forces and high cutting temperatures.In this paper,the true stress-strain curve of Inconel 718 at room temperature was obtained by the split Hopkinson pressure bar experiment,and the thermal softening rate of the material at different temperatures was obtained by the high-temperature hardness experiment.The laser thermal conductivity experiment was used to obtain the specific heat capacity and thermal conductivity of Inconel 718 at different temperatures,and the actual deformation temperatures at different strains were calculated by combining the true stress-strain curves.The decoupling of strain and temperature is achieved by using the thermal softening rate to correct the true stress-strain curve in the variable temperature state to the stress-strain curve in the isothermal state.The above experimental results were fitted based on the Johnson-Cook and Power-Law constitutive models,and the results show that the fitting accuracy of the Power-Low constitutive model is higher at low strain rates,while that of the Johnson-Cook constitutive model is higher at high strain rates.Finally,the response mechanism of the mechanical properties of Inconel 718 material under the action of strain,strain rate and temperature alone are explored through finite element simulation,and it is found that the strain has the greatest influence on the stress,followed by the temperature,and the strain rate has basically no influence on the stress.

Inconel 718Isothermal stress-strain curvesConstitutive modelFinite element simulationMechanical response

姜峰、李金鑫、徐军、沈哲明、姚红飞、朱冬伟、曾祥申、张超、张涛

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华侨大学制造工程研究院,厦门 361021

高性能工具全国重点实验室,厦门 361021

浙江欣兴工具有限公司,嘉兴 314300

华侨大学机电及自动化学院,厦门 361021

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Inconel 718 等温应力-应变曲线 本构模型 有限元仿真 力学响应

国家重点研发计划国家自然科学基金面上项目

2023YFB340720052275428

2024

航空制造技术
北京航空制造工程研究所

航空制造技术

CSTPCD北大核心
影响因子:0.403
ISSN:1671-833X
年,卷(期):2024.67(8)
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