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高温高应变率下GH4169合金本构模型的构建

张继林 唐林虎 马富荣 李忠林 哈金福

张继林, 唐林虎, 马富荣, 李忠林, 哈金福. 高温高应变率下GH4169合金本构模型的构建[J]. 钢铁钒钛, 2025, 46(3): 157-166. doi: 10.7513/j.issn.1004-7638.2025.03.022
引用本文: 张继林, 唐林虎, 马富荣, 李忠林, 哈金福. 高温高应变率下GH4169合金本构模型的构建[J]. 钢铁钒钛, 2025, 46(3): 157-166. doi: 10.7513/j.issn.1004-7638.2025.03.022
ZHANG Jilin, TANG Linhu, MA Furong, LI Zhonglin, HA Jinfu. Construction of constitutive model for GH4169 alloy under high temperature and high strain rate[J]. IRON STEEL VANADIUM TITANIUM, 2025, 46(3): 157-166. doi: 10.7513/j.issn.1004-7638.2025.03.022
Citation: ZHANG Jilin, TANG Linhu, MA Furong, LI Zhonglin, HA Jinfu. Construction of constitutive model for GH4169 alloy under high temperature and high strain rate[J]. IRON STEEL VANADIUM TITANIUM, 2025, 46(3): 157-166. doi: 10.7513/j.issn.1004-7638.2025.03.022

高温高应变率下GH4169合金本构模型的构建

doi: 10.7513/j.issn.1004-7638.2025.03.022
基金项目: 甘肃省教育厅产业支撑计划项目(2022CYZC-68);甘肃省高等学校创新基金项目(2021B-319);兰州工业学院青年科技创新项目(2024KJ-23)。
详细信息
    作者简介:

    张继林,男,1987年出生,甘肃民乐人,硕士,副教授,主要从事金属材料的动态力学性能及切削性能研究,E-mail:zjl-0111@163.com

    通讯作者:

    唐林虎,男,1978年出生,甘肃武山人,博士,教授,主要从事金属材料力学性能、切削性能及摩擦学领域研究,E-mail:314364973@qq.com

  • 中图分类号: TG132.3,TG115.5

Construction of constitutive model for GH4169 alloy under high temperature and high strain rate

  • 摘要: 利用万能试验机(UTM5305)和霍普金森动态试验装置(ALT 1000)对GH4169合金分别进行准静态压缩试验和动态冲击试验,获得常温下应变率为0.001、0.003、0.1 s−1的准静态试验数据;以及温度为25、600、750、900 ℃和应变率为1500250035004500 s−1的动态试验数据,构建了Johnson-Cook(JC)本构模型及其修正模型。研究显示,材料的塑性硬化、热软化和速率敏感性都得到了体现,尤其在温度升至900 ℃时,软化效应尤为突出;原始JC本构方程的相关系数(r)为0.9147,决定系数(R2)为0.7422,平均相对误差(AARE)为14.53%,修正后的JC本构方程相关系数(r)提高至0.9444,决定系数(R2)提高至0.8867,平均相对误差(AARE)下降至10.77%,相较原始JC本构模型在预测精度和可靠性方面有显著提升,能够可靠正确描述材料的应力-应变行为。
  • 图  1  准静态条件下高温合金GH4169的真实应力-真应变曲线

    Figure  1.  True stress-true strain curve of superalloy GH4169 under quasi-static conditions

    图  2  高温合金GH4169 25、600、750、900 ℃的真应力-应变曲线

    (a) T=25 ℃; (b) T =600 ℃; (c) T =750 ℃; (d) T =900 ℃

    Figure  2.  True stress-strain curves for high temperature alloy GH4169 at different temperatures

    图  4  屈服强度

    Figure  4.  Yield stress of experimental steel

    图  3  高温合金GH4169 1500250035004500 s−1的真应力-应变曲线

    (a) $ \dot{\varepsilon}=1\ 500\text{ }\text{s}^{-1} $; (b) $ \dot{\varepsilon}=2\ 500\text{ }\text{s}^{-1} $; (c) $ \dot{\varepsilon}=3\ 500\text{ }\text{s}^{-1} $ ; (d) $ \dot{\varepsilon}=4\ 500\text{ }\text{s}^{-1} $

    Figure  3.  True stress-strain curves for high-temperature alloy GH4169 under different strain rates

    图  5  $ \ln (\sigma - A) $和$ \ln \varepsilon $的关系

    Figure  5.  Relationship between $ \ln (\sigma - A) $ and $ \ln \varepsilon $

    图  6  J-C本构方程参数$ C $和应变率$ \dot \varepsilon $拟合关系

    Figure  6.  Fitting diagram of the relationship between J-C constitutive equation parameters $ C $ and strain rate $ \dot \varepsilon $

    图  7  J-C本构方程参数$ m $和温度$ T $拟合关系

    Figure  7.  Fitting diagram of the relationship between parameters $ m $ and temperature $ T $ of the J-C constitutive equation

    图  8  两种本构模型的真应力预测和试验值比较

    黑色:25℃;红色:600℃;蓝色:750℃;紫色:900℃(a)$ \dot{\varepsilon}=1\ 500\text{ }\text{s}^{-1} $ ; (b) $ \dot{\varepsilon}=2\ 500\text{ }\text{s}^{-1} $;(c) $ \dot{\varepsilon}=3\ 500\text{ }\text{s}^{-1} $ ; (d) $ \dot{\varepsilon}=4\ 500\text{ }\text{s}^{-1} $

    Figure  8.  Comparison of true stress predictions and experimental values for two constitutive models

    图  9  两种本构模型的相关系数(r)、决定系数(R2)和平均相对误差(AARE)

    (a)原JC本构模型;(b)修正JC本构模型

    Figure  9.  Correlation coefficient (r), determination coefficient (R2) and average relative error (AARE) of the two constitutive models

    表  1  25、600、750、900 ℃下GH4169合金材料不同应变率时的屈服强度

    Table  1.   Yield strength of GH4169 alloy at different strain rates at 25, 600, 750 and 900 ℃

    温度/℃应变率/s−1屈服强
    度/MPa
    塑性流动
    段应变
    失效
    应变
    失效应
    力/MPa
    2515001221.300.07470.07611263.98
    25001240.020.20280.2130931.75
    35001305.970.33900.36111020.32
    45001404.720.43570.44751535.05
    6001500900.830.20790.2106898.18
    25001000.460.22540.23451062.14
    35001054.440.34340.35571058.25
    45001085.020.31010.3541595.29
    7501500891.210.17090.1756974.66
    2500910.310.27650.2987579.53
    3500950.690.36930.3868872.06
    4500979.470.47490.4910820.53
    9001500350.860.16050.1632458.72
    2500380.280.25190.2578708.53
    3500401.320.37180.3793632.80
    4500420.200.45060.4560766.36
    下载: 导出CSV

    表  2  不同应变率下加工硬化参数(25、600、750、900 ℃下)

    Table  2.   Work hardening parameters at different strain rates for temperatures of 25, 600, 750, and 900 ℃

    温度/℃ k n
    1500 s−1 2500 s−1 3500 s−1 4500 s−1 1500 s−1 2500 s−1 3500 s−1 4500 s−1
    25 3289 1327 1098 862 0.78 0.61 0.70 0.61
    600 1655 1920 1386 2536 0.67 0.70 0.71 1.20
    750 2430 2131 2207 1153 0.84 0.99 1.05 0.84
    900 4622 2188 1 918 1769 1.24 0.93 0.94 0.88
    下载: 导出CSV

    表  3  GH4169合金传动J-C本构模型参数C的值

    Table  3.   Values of parameter C of the J-C constitutive model of GH4169 alloy transmission

    $ T $/℃应变率$ \dot \varepsilon $/s−1屈服强度$ \sigma $/MPa参数$ C $值参数$ C $平均值
    2515001175.100.00810.0127
    25001305.080.0091
    35001471.960.0135
    45001618.270.0201
    下载: 导出CSV

    表  4  GH4169合金传动J-C本构模型参数m的值

    Table  4.   Values of parameter m of the J-C constitutive model of GH4169 alloy transmission

    应变率$ \dot \varepsilon $/s−1温度$ T $/℃屈服应力$ \sigma $/MPa参数$ m $值参数$ m $平均值
    1500600900.831.49311.8429
    750891.212.0468
    900350.860.8153
    25006001054.432.0961
    750950.692.3037
    900401.320.9510
    35006001187.943.0772
    7501048.922.8663
    900355.530.8192
    45006001085.022.2265
    750979.472.4221
    900420.200.9978
    下载: 导出CSV

    表  5  GH4169合金的修正J-C本构模型参数值

    Table  5.   Parameters of modified J-C constitutive model for GH4169 alloy

    $ A $/MPa $ B $/MPa $ n $ $ {C_1} $ $ {C_2} $ $ {m_1} $ $ {m_2} $
    1113.84 645.69 0.34674 0.0006 4.0301×10−6 5.16143 0.00442
    下载: 导出CSV
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    ZHAO L D, ZHANG Y M, ZHANG J L, et al. Research on prediction accuracy of the flow stress of 0Cr17Ni4Cu4Nb stainless steel based on machine learning[J]. Iron Steel Vanadium Titanium, 2023, 44 (4): 196-204.
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出版历程
  • 收稿日期:  2024-06-10
  • 网络出版日期:  2025-06-30
  • 刊出日期:  2025-06-30

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