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基于双向拉伸的热环境铝合金性能获取和分析

房涛涛 李晓星 肖瑞

房涛涛, 李晓星, 肖瑞等 . 基于双向拉伸的热环境铝合金性能获取和分析[J]. 北京航空航天大学学报, 2019, 45(6): 1195-1202. doi: 10.13700/j.bh.1001-5965.2018.0625
引用本文: 房涛涛, 李晓星, 肖瑞等 . 基于双向拉伸的热环境铝合金性能获取和分析[J]. 北京航空航天大学学报, 2019, 45(6): 1195-1202. doi: 10.13700/j.bh.1001-5965.2018.0625
FANG Taotao, LI Xiaoxing, XIAO Ruiet al. Acquisition and analysis of aluminum alloy property in thermal environment based on biaxial tension[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1195-1202. doi: 10.13700/j.bh.1001-5965.2018.0625(in Chinese)
Citation: FANG Taotao, LI Xiaoxing, XIAO Ruiet al. Acquisition and analysis of aluminum alloy property in thermal environment based on biaxial tension[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1195-1202. doi: 10.13700/j.bh.1001-5965.2018.0625(in Chinese)

基于双向拉伸的热环境铝合金性能获取和分析

doi: 10.13700/j.bh.1001-5965.2018.0625
基金项目: 

国家自然科学基金 5171101484

详细信息
    作者简介:

    房涛涛  女, 博士研究生。主要研究方向:数字化板料成形技术

    李晓星  男, 博士, 教授, 博士生导师。主要研究方向:数字化板料成形技术

    通讯作者:

    李晓星, E-mail: li.xiaoxing@buaa.edu.cn

  • 中图分类号: V260.5;TG166.3

Acquisition and analysis of aluminum alloy property in thermal environment based on biaxial tension

Funds: 

National Natural Science Foundation of China 5171101484

More Information
  • 摘要:

    板材成形加工时通常承受复杂载荷,一般采用单拉试验获取材料性能,由于材料变形时仅承受单向载荷,与实际情况差距较大。为获取更加真实的复杂加载时材料性能,通过十字形试件双向拉伸试验,研究了热环境双向变比例加载时AA6016铝合金材料力学性能和变形行为,包括优化设计十字形试件、相关试验方法和设备以及结果分析等。在25、150和250℃温度下进行了拉伸速率比例为1:1、3:2、2:3、1:3和3:1的双向拉伸试验和单向拉伸试验,得到了不同拉伸速率比例和温度下的应力应变关系、屈服规律和各向异性,建立了屈服准则,并且通过与试验结果对比,讨论分析了几个典型屈服准则及其适用性。

     

  • 图 1  铝合金试件尺寸

    Figure 1.  Dimensions of aluminium alloy specimen

    图 2  热环境双向拉伸试验机[18]

    Figure 2.  Biaxial tensile test machine in thermal environment[18]

    图 3  喷上散斑的零件及第一主应变

    Figure 3.  Speckle-sprayed component and major principal strain diagram

    图 4  不同温度下5种行程比例的应力应变曲线

    Figure 4.  Stress-strain curves of five stroke ratios under different temperatures

    图 5  25、150、250℃下5种行程比例的应力应变曲线

    Figure 5.  Stress-strain curves of five stroke ratios at 25, 150 and 250℃

    图 6  AA6016铝合金单向拉伸应力应变曲线

    Figure 6.  AA6016 aluminum alloy stress-strain curves of uniaxial tension

    图 7  屈服轨迹和相关试验的关系

    Figure 7.  Relationship between yield trajectory and relevant tests

    图 8  塑性功原理

    Figure 8.  Plastic work principle

    图 9  0.2%等效应变下的屈服轨迹

    Figure 9.  Yield trajectories under 0.2% equivalent strain

    图 10  1%等效应变下的屈服轨迹

    Figure 10.  Yield trajectories under 1% equivalent strain

    表  1  AA6016铝合金各向异性系数

    Table  1.   Anisotropy coefficient of AA6016 aluminium alloy

    T/℃ r0 r45 r90 r
    25 0.87 0.46 0.73 0.63
    150 1.22 0.65 0.96 0.87
    250 1.86 1.03 1.29 1.302 5
    注:T为试验温度。
    下载: 导出CSV
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出版历程
  • 收稿日期:  2018-10-31
  • 录用日期:  2018-11-23
  • 网络出版日期:  2019-06-20

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