双面爆炸焊接的数值模拟

缪广红 李亮 江向阳 刘文震 李雪交 汪泉 余勇 沈兆武

缪广红, 李亮, 江向阳, 刘文震, 李雪交, 汪泉, 余勇, 沈兆武. 双面爆炸焊接的数值模拟[J]. 高压物理学报, 2018, 32(4): 045202. doi: 10.11858/gywlxb.20180513
引用本文: 缪广红, 李亮, 江向阳, 刘文震, 李雪交, 汪泉, 余勇, 沈兆武. 双面爆炸焊接的数值模拟[J]. 高压物理学报, 2018, 32(4): 045202. doi: 10.11858/gywlxb.20180513
MIAO Guanghong, LI Liang, JIANG Xiangyang, LIU Wenzhen, LI Xuejiao, WANG Quan, YU Yong, SHEN Zhaowu. Numerical Simulation of Double-Sided Explosive Welding[J]. Chinese Journal of High Pressure Physics, 2018, 32(4): 045202. doi: 10.11858/gywlxb.20180513
Citation: MIAO Guanghong, LI Liang, JIANG Xiangyang, LIU Wenzhen, LI Xuejiao, WANG Quan, YU Yong, SHEN Zhaowu. Numerical Simulation of Double-Sided Explosive Welding[J]. Chinese Journal of High Pressure Physics, 2018, 32(4): 045202. doi: 10.11858/gywlxb.20180513

双面爆炸焊接的数值模拟

doi: 10.11858/gywlxb.20180513
基金项目: 

国家自然科学基金 51374189

国家自然科学基金 11502001

安徽省高校自然科学基金重点项目 KJ2017A089

安徽省高校自然科学基金重点项目 KJ2018A0090

安徽省自然科学基金 1708085QA17

安徽省自然科学基金 1808085QA06

详细信息
    作者简介:

    缪广红(1985-), 男, 博士, 讲师, 主要从事含能材料、爆炸复合及爆炸力学相关领域研究.E-mail:miaogh@mail.ustc.edu.cn

  • 中图分类号: O389;TJ55

Numerical Simulation of Double-Sided Explosive Welding

  • 摘要: 双面爆炸焊接一次起爆可同时焊接两组复合板,而且使炸药临界厚度显著降低,提高了炸药的能量利用率,解决了爆炸焊接现存的高噪低效问题。借助ANSYS/LS-DYNA动力学分析软件,运用光滑粒子流体动力学方法(SPH)与有限元(FEM)耦合算法,对双面爆炸焊接进行了三维数值模拟,并将模拟结果与实验结果和理论计算结果进行了对比。结果表明,数值模拟结果与实验结果较吻合,且与Deribas的理论计算结果一致性较好,说明Deribas公式和SPH-FEM耦合方法对双面爆炸焊接具有较好的指导意义。

     

  • 图  计算模型Ⅰ(10 mm药厚)

    Figure  1.  Calculation model Ⅰ with explosive thickness of 10 mm

    图  计算模型Ⅱ(5 mm药厚)

    Figure  2.  Calculation model Ⅱ with explosive thickness of 5 mm

    图  10 mm药厚下爆炸焊接结束时复板的z向位移云图

    Figure  3.  z-direction displacement contour of flyer plate with explosive thickness of 10 mm at the end of explosive welding

    图  10 mm药厚下复板上3个特征单元的z向位移-时间历程

    Figure  4.  z-direction displacement histories of 3 characteristic elements with explosive thickness of 10 mm

    图  10 mm药厚下的一对特征单元

    Figure  5.  A pair of characteristic elements with explosive thickness of 10 mm

    图  一对特征单元(见图 5)的速度-时间曲线

    Figure  6.  Velocity-time curves of the pair of characteristic elements (see Fig. 5)

    图  10 mm药厚下复板结合界面处的3个特征单元

    Figure  7.  3 characteristic elements at the bonding interface of flyer plate with explosive thickness of 10 mm

    图  10 mm药厚下3个特征单元的速度-时间曲线

    Figure  8.  Velocity-time curves of 3 characteristic elements with explosive thickness of 10 mm

    图  10 mm药厚下复板结合界面处的3个特征单元

    Figure  9.  3 characteristic elements at the bonding interface of flyer plate with explosive thickness of 10 mm

    图  10  10 mm药厚下3个特征单元的压力-时间曲线

    Figure  10.  Pressure-time curves of 3 characteristic elements with explosive thickness of 10 mm

    图  11  5 mm药厚下爆炸复合结束时复板的z向位移云图

    Figure  11.  z-displacement contour of flyer plate with explosive thickness of 5 mm at the end of explosive welding

    图  12  5 mm药厚下复板上特征单元的z向位移-时间历程

    Figure  12.  z-displacement histories of 3 characteristic elements with explosive thickness of 5 mm

    图  13  5 mm药厚下的一对特征单元

    Figure  13.  A pair of characteristic elements with explosive thickness of 5 mm

    图  14  一对特征单元(见图 13)的速度-时间曲线

    Figure  14.  Velocity-time curves of the pair of characteristic elements (see Fig. 13)

    图  15  5 mm药厚下复板结合界面处的3个特征单元

    Figure  15.  3 characteristic elements at the bonding interface of flyer plate with explosive thickness of 5 mm

    图  16  5 mm药厚下3个特征单元的速度-时间曲线

    Figure  16.  Velocity-time curves of 3 characteristic elements with explosive thickness of 5 mm

    图  17  5 mm药厚下复板结合界面处的3个特征单元

    Figure  17.  3 characteristic elements at the bonding interface of flyer plate with explosive thickness of 5 mm

    图  18  5 mm药厚下3个特征单元的压力历程

    Figure  18.  Pressure histories of 3 characteristic elements with explosive thickness of 5 mm

    表  1  计算模型中材料的相关参数

    Table  1.   Related parameters of materials in calculation models

    Calculationmodel Flyer plate Base plate Gap
    δ/mm
    Size of explosive/(mm×mm×mm)
    Material Size/(mm×mm×mm) Material Size/(mm×mm×mm)
    45 steel 300×150×2 Q235 300×150×16 6 300×150×10
    45 steel 300×150×2 Q235 300×150×16 6 300×150×5
    下载: 导出CSV

    表  2  乳化炸药的JWL状态参数[13]

    Table  2.   JWL equation-of-state parameters of emulsion explosives[13]

    ρ/(g·cm-3) D/(m·s-1) AJWL/GPa BJWL/GPa R1 R2 ω E0/(kJ·cm-3)
    1.12 4 510 326.42 5.808 9 5.80 1.56 0.57 3.323
    下载: 导出CSV

    表  3  Q235钢的Johnson-Cook模型参数[16]

    Table  3.   Johnson-Cook parameters of Q235 steel[16]

    ρ/(g·cm-3) G/GPa A/GPa B/GPa C n m Tm/K Tr/K
    7.83 77 0.792 0.51 0.014 0.26 1.03 1 793 294
    下载: 导出CSV

    表  4  10 mm药厚下碰撞速度理论计算结果与数值模拟结果的比较

    Table  4.   Comparison of collision velocity between theoretical calculation and numerical simulation with explosive thickness of 10 mm

    Theoreticalformula Massfraction Collision velocity/(m·s-1) Error/%
    Theoretical calculation[18] Simulation
    Gurney 0.75 1 089 897 -21.0
    Aziz 0.75 711 897 20.0
    Deribas 0.75 853 897 4.9
    下载: 导出CSV

    表  5  5 mm药厚下碰撞速度理论计算结果与数值模拟结果的比较

    Table  5.   Comparison of collision velocity between theoretical calculation and numerical simulation with explosive thickness of 5 mm

    Theoreticalformula Massfraction Collision velocity/(m·s-1) Error/%
    Theoretical calculation[18] Simulation
    Gurney 0.45 863 565 -52.7
    Aziz 0.45 480 565 15.0
    Deribas 0.45 576 565 -1.9
    下载: 导出CSV

    表  6  10 mm药厚下碰撞压力理论计算结果与数值模拟结果的比较

    Table  6.   Comparison of collision pressure betweentheoretical calculation and numerical simulationwith explosive thickness of 10 mm

    Theoreticalformula Collision pressure/GPa Error/%
    Calculation Simulation
    Gurney 22.08 17.08 -29.3
    Aziz 14.42 17.08 15.6
    Deribas 17.30 17.08 -1.3
    下载: 导出CSV

    表  7  5 mm药厚下碰撞压力理论计算结果与数值模拟结果的比较

    Table  7.   Comparison of collision pressure betweentheoretical calculation and numerical simulationwith explosive thickness of 5 mm

    Theoreticalformula Collision pressure/GPa Error/%
    Calculation Simulation
    Gurney 17.50 11.25 -55.6
    Aziz 9.73 11.25 13.5
    Deribas 11.68 11.25 -3.8
    下载: 导出CSV
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  • 收稿日期:  2018-02-01
  • 修回日期:  2018-03-02

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