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材料超高温动态拉伸SHTB实验方法的有效性分析

李鹏辉 郭伟国 刘开业 王建军 谭学明

孙承纬. 爆轰理论导引[J]. 爆炸与冲击, 1987, 7(3): 278-278. doi: 10.11883/1001-1455(1987)03-0278-1
引用本文: 李鹏辉, 郭伟国, 刘开业, 王建军, 谭学明. 材料超高温动态拉伸SHTB实验方法的有效性分析[J]. 爆炸与冲击, 2018, 38(2): 426-436. doi: 10.11883/bzycj-2016-0259
LI Penghui, GUO Weiguo, LIU Kaiye, WANG Jianjun, TAN Xueming. Validity analysis of materials' dynamic tensile SHTB experimental technique at ultrahigh temperature[J]. Explosion And Shock Waves, 2018, 38(2): 426-436. doi: 10.11883/bzycj-2016-0259
Citation: LI Penghui, GUO Weiguo, LIU Kaiye, WANG Jianjun, TAN Xueming. Validity analysis of materials' dynamic tensile SHTB experimental technique at ultrahigh temperature[J]. Explosion And Shock Waves, 2018, 38(2): 426-436. doi: 10.11883/bzycj-2016-0259

材料超高温动态拉伸SHTB实验方法的有效性分析

doi: 10.11883/bzycj-2016-0259
基金项目: 

国家自然科学基金项目 11372255

国家自然科学基金项目 11572261

详细信息
    作者简介:

    李鹏辉(1991—),男,硕士

    通讯作者:

    郭伟国, weiguo@nwpu.edu.cn

  • 中图分类号: O344.3

Validity analysis of materials' dynamic tensile SHTB experimental technique at ultrahigh temperature

  • 摘要: 针对高温拉伸分离式Hopkinson杆实验技术,通过数值模拟、实验验证以及几种典型材料的高温动态拉伸性能测试相结合的方法,对此实验技术中存在的几个关键问题进行了深入研究。结果表明:对于平板状钩挂式拉伸试样,通过标距段尺寸优化后,应力分布均匀,流动应力曲线与螺纹拉伸试样一致,且应力上升段后没有剧烈跳动;通过精确气动控制,在加载脉冲到来同时,可实现有效的试样快速同步组装和加载;当试样温度为1 200 ℃时,在冷加载杆与高温试样接触以及应力波加载试样的整个过程中,试样平均温度下降约1.3%,而加载杆端温升低于180 ℃。为了验证此实验技术,对3D打印TC4、镍基单晶高温合金DD6进行了最高温度约1 200 ℃时的高温动态拉伸力学性能实验测试。
  • 图  1  SHTB试样连接形式

    Figure  1.  Connection forms of SHTB specimen

    图  2  高温SHTB实验过程示意图

    Figure  2.  Schematic diagram of SHTB experimental process at high temperature

    图  3  高温SHTB实验装置示意图

    Figure  3.  Illustration of setup for high temperature SHTB experiment

    图  4  数值模拟流动应力曲线与输入曲线对比

    Figure  4.  Comparison of simulated flow stress curve with input curves

    图  5  钩挂式平板试样尺寸设计

    Figure  5.  Size design of hook joint flat specimen

    图  6  试样尺寸对流动应力曲线的影响

    Figure  6.  Effect of specimen size on flow stress curve

    图  7  钩挂式板状试样不同长宽比下应力和应变分布

    Figure  7.  Flat hook-joint specimen's stress and strain distribution at different ratios of length to width

    图  8  钩挂连接与螺纹连接数值模拟和实验结果对比

    Figure  8.  Comparison of numerical simulation and experimental results between hook joint and thread connection

    图  9  钛合金TC4弹性模量随温度变化

    Figure  9.  Elastic modulus of titanium alloy TC4 versus temperature

    图  10  冷接触时间示意图

    Figure  10.  Cold contact time

    图  11  冷接触时间测试

    Figure  11.  Cold contact time measurement

    图  12  热辐射和热对流过程沿宽度和厚度方向温度分布

    Figure  12.  Temperature distribution along width and thickness

    图  13  冷接触过程试样中线温度分布

    Figure  13.  Temperature distribution along center line of specimen during cold contact

    图  14  热辐射、热对流和热传导对标距段平均温度的影响

    Figure  14.  Effect of heat radiation, heat convection and heat conduction on average temperature

    图  15  标距段温度下降随试样初始温度变化

    Figure  15.  Average temperature of gage section drop versus specimen initial temperature

    图  16  不同加热温度引起的加载杆端温升

    Figure  16.  Temperature rise of loading bars caused by different heating temperatures

    图  17  典型材料的动态拉伸真实应力-应变曲线

    Figure  17.  Dynamic true tress versus true strain

    表  1  钛合金TC4弹性模量的变化幅度

    Table  1.   Variation of elastic modulus of titanium alloy TC4

    T/℃ |δE|/%
    Ref.[12] Ref.[13]
    100 0.5 1.0
    200 4.2 3.5
    300 6.0 10.1
    400 10.3 20.0
    500 22.9 37.0
    600 24.4 62.6
    700 28.0
    800 37.7
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出版历程
  • 收稿日期:  2016-08-24
  • 修回日期:  2017-01-18
  • 刊出日期:  2018-03-25

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