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2024-T3航空铝合金板材电磁V形弯曲应变分析

熊威人 王文平 万敏 李新军

熊威人, 王文平, 万敏, 等 . 2024-T3航空铝合金板材电磁V形弯曲应变分析[J]. 北京航空航天大学学报, 2016, 42(1): 158-164. doi: 10.13700/j.bh.1001-5965.2015.0075
引用本文: 熊威人, 王文平, 万敏, 等 . 2024-T3航空铝合金板材电磁V形弯曲应变分析[J]. 北京航空航天大学学报, 2016, 42(1): 158-164. doi: 10.13700/j.bh.1001-5965.2015.0075
XIONG Weiren, WANG Wenping, WAN Min, et al. Analysis of strain in electromagnetic V-shaped bending of 2024-T3 aviation aluminum alloy plate[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1): 158-164. doi: 10.13700/j.bh.1001-5965.2015.0075(in Chinese)
Citation: XIONG Weiren, WANG Wenping, WAN Min, et al. Analysis of strain in electromagnetic V-shaped bending of 2024-T3 aviation aluminum alloy plate[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1): 158-164. doi: 10.13700/j.bh.1001-5965.2015.0075(in Chinese)

2024-T3航空铝合金板材电磁V形弯曲应变分析

doi: 10.13700/j.bh.1001-5965.2015.0075
基金项目: 国家"973"计划(2011CB012800,2011CB012804)
详细信息
    作者简介:

    熊威人男,博士研究生。主要研究方向:基于电磁成形技术的航空板材成形方法。Tel.:010-82338613E-mail:wudiguixu@163.com;万敏男,博士,教授,博士生导师。主要研究方向:新材料成形理论与技术、先进成形工艺与装备技术、飞机数字化制造技术与系统。Tel.:010-82338788E-mail:mwan@buaa.edu.cn

    通讯作者:

    万敏,Tel.:010-82338788E-mail:mwan@buaa.edu.cn

  • 中图分类号: V261.7+1;TB31

Analysis of strain in electromagnetic V-shaped bending of 2024-T3 aviation aluminum alloy plate

Funds: National Basic Research Program of China (2011CB012800,2011CB012804)
  • 摘要: 金属塑性成形后的应变特征影响零件的力学性能和使用寿命。电磁成形技术能提高金属的成形性,有助于克服铝合金室温成形性低的缺点,因而得到重视。本文以2024-T3航空铝合金板为研究对象,开展了电磁V弯成形和传统机械V弯成形的实验及数值模拟,研究了2种成形方法对弯曲成形试件V形弯曲圆角位置沿试件长度方向的应变特征的影响。数值模型表明,电磁V弯试件弯曲圆角处的拉应变峰值低于机械V弯试件;电磁V弯实验件的拉应变峰值比机械V弯试件低13.9%。同时,与机械V弯试件相比,电磁V弯试件有更大区域的金属材料参与了弯曲变形。

     

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出版历程
  • 收稿日期:  2015-02-04
  • 网络出版日期:  2016-01-20

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