杨俊茹,徐昊,王桂杰,朱然,邓大祥,吴清源.基于Python的Abaqus二次开发在高温合金GH3039激光冲击强化中的应用[J].表面技术,2023,52(7):435-443.
#$NPYANG Jun-ru,XU Hao,WANG Gui-jie,ZHU Ran,DENG Da-xiang,WU Qing-yuan.Application of Python-based Abaqus Redevelopment in Laser Shock Peening of Superalloy GH3039[J].Surface Technology,2023,52(7):435-443
基于Python的Abaqus二次开发在高温合金GH3039激光冲击强化中的应用
Application of Python-based Abaqus Redevelopment in Laser Shock Peening of Superalloy GH3039
  
DOI:10.16490/j.cnki.issn.1001-3660.2023.07.040
中文关键词:  Abaqus二次开发  Python  激光冲击强化  残余压应力  光斑直径  激光能量  冲击次数
英文关键词:redevelopment of Abaqus  Python  laser shock peening  residual compressive stress  spot diameter  laser energy  impact times
基金项目:浙江省城市轨道交通智能运维技术与装备重点实验室开放课题基金(ZSDRTKF2021002);深圳市自然科学基金基础研究重点项目(JCYJ20200109112808109);中国博士后科学基金(2020M682617);广东省基础与应用基础研究基金(2020A1515011553);国家自然科学基金(52105463);山东省自然科学基金(ZR2020QE182,ZR2022ME150,ZR2022ME129)
作者单位
杨俊茹 山东科技大学,山东 青岛 266590 
徐昊 山东科技大学,山东 青岛 266590 
王桂杰 山东科技大学,山东 青岛 266590 
朱然 山东科技大学,山东 青岛 266590;浙江省城市轨道交通智能运维技术与装备重点实验室,浙江 金华 321004 
邓大祥 哈尔滨工业大学深圳,广东 深圳 518055 
吴清源 广东工业大学,广州 510006 
AuthorInstitution
#$NPYANG Jun-ru Shandong University of Science and Technology, Shandong Qingdao 266590, China 
XU Hao Shandong University of Science and Technology, Shandong Qingdao 266590, China 
WANG Gui-jie Shandong University of Science and Technology, Shandong Qingdao 266590, China 
ZHU Ran Shandong University of Science and Technology, Shandong Qingdao 266590, China;Key Laboratory of Urban Rail Transit Intelligent Operation and Maintenance Technology & Equipment of Zhejiang Province, Zhejiang Jinhua 321004, China 
DENG Da-xiang Harbin Institute of Technology Shenzhen, Guangdong Shenzhen 518055, China 
WU Qing-yuan Guangdong University of Technology, Guangzhou 510006, China 
摘要点击次数:
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中文摘要:
      目的 提高高温合金GH3039激光冲击强化仿真建模的效率。方法 利用Python脚本语言对Abaqus进行二次开发,利用插件对高温合金GH3039激光冲击强化过程进行仿真分析。采用侧倾固定Ψ法,通过实验测量激光冲击强化后的残余应力,并对仿真结果进行验证,分析不同激光工艺参数作用下高温合金GH3039表面和深度方向残余应力的分布规律。结果 仿真插件界面简洁,操作性强,结果准确。在其他参数不变的情况下,残余压应力受到光斑尺寸的影响较大。相较于光斑直径为4、2 mm,在光斑直径为6 mm时,其中心位置残余压应力分别提高了4.3%、53%。随着光斑尺寸的增大,表面残余压应力增大,且变化梯度减小,深度方向的残余压应力增大。随着激光能量的增加,表面残余压应力增大,且变化梯度增大,残余压应力峰值位于中心区域附近,在激光能量为6、7、8 J时,残余压应力层的平均厚度分别为0.55、0.67、0.82 mm,深度方向残余压应力层增厚。随着冲击次数的增加,冲击区域表面残余压应力平均值高于单次冲击,且波动梯度增大,冲击1、2、3次后残余压应力层的平均厚度分别为0.55、0.71、0.85 mm,深度方向残余压应力层深度增大。结论 利用Python脚本语言对ABAQUS进行二次开发,提高了仿真建模的效率,可为快速预测不同激光工艺参数下高温合金GH3039残余应力的分布规律提供参考。
英文摘要:
      In the simulation process of laser shock peening of superalloy GH3039 with different laser process parameters, one or several laser parameters need to be frequently changed for repeated modeling, which reduces the efficiency of simulation. The method of redevelopment of Abaqus with Python script can realize the parametric modeling of simulation process and significantly improve the efficiency of simulation analysis. With superalloy GH3039 as the research object, a simulation plug-in for laser shock peening of superalloy GH3039 was established by Python language, and the correctness of the plug-in results was verified by experiments. Through the comparison between the experimental results and the simulation data, it was known that the plug-in simulation results had high accuracy. Based on this plug-in, the distribution of residual stress in superalloy GH3039 with different laser process parameters was studied, and the distribution of residual stress in surface direction and depth direction of superalloy GH3039 with different laser spot sizes, laser energy and laser impact times was analyzed. The spot size had a greater effect on the distribution law of residual stress in the surface direction. Compared with the maximum residual stress under the spot diameter of 4 mm and 2 mm, the maximum residual stress under the spot diameter of 6 mm increased by 4.3% and 53% respectively. With the increase of the spot size, the residual compressive stress in the surface direction increased and the variation gradient decreased, and the residual compressive stress in the depth direction increased. This was because the large spot transmitted the shock wave in the form of plane wave and small spot transmitted shock wave in the form of spherical wave, while plane wave attenuated slowly when transmitting laser energy. With the increase of energy, the peak value of laser shock wave pressure changed. On the premise that other process parameters remained unchanged, the superalloy GH3039 was subject to laser shock peening with 6 J, 7 J and 8 J laser energy respectively, and the peak pressure was 2.3 GPa, 2.5 GPa and 2.68 GPa respectively. The average value of residual compressive stress in the impact area increased with the increase of laser energy, and the fluctuation gradient of residual compressive stress increased. The peak value of residual compressive stress was near the central region. This was because the surface wave of the circular spot converged to the center of the laser impact area, causing local reverse plastic strain and reducing the residual compressive stress level. The average depth of the plastic layer subject to 6 J, 7 J and 8 J laser energy was 0.55 mm, 0.67 mm and 0.82 mm, and the depth of the plastic layer increased. The samples were impacted once, twice and three times at the same position respectively. The average value of residual compressive stress in the surface direction of multiple impact peening was higher than that of single impact peening, but the difference was small between the average value of residual compressive stress in the second impact and the third impact. This was because the material was hardened after laser impact peening. With the increase of impact times, the degree of hardening and the fluctuation gradient of residual compressive stress both became larger. With the increase of impact times, the residual compressive stress increased. The average depth of plastic layer impacted once, twice and three times was 0.55 mm, 0.71 mm and 0.85 mm. Multiple impacts can increase the depth of plastic layer.
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