喷丸弹坑应力场演变的相似性实验与仿真模拟Similarity experiment and simulation of stress field evolution in shot peening craters
胡俊,廖凯,罗鹏博,李立君,陈飞
摘要(Abstract):
运用ANSYS动力学模块建立单弹坑、双弹坑交叠模型和三弹坑互交模型,分析材料表面在弹丸作用下的动态塑变过程和弹坑形变与应力场分布规律。鉴于实际弹坑无法直接测试,实验基于相似原则,放大弹丸和坑型尺度,通过X射线衍射(XRD)表面应力测试获得弹坑应力分布,将结果归一化处理后与喷丸仿真下弹坑应力分布规律进行对比。结果表明:相似性实验结果与仿真结果具有较好的一致性;单弹坑内呈压应力分布,应力大小与形变量直接相关,从坑沿到凹陷最深处,应力强度逐渐增大;1/4d(d为弹丸直径)偏置模型中,弹丸依次撞击靶材,弹坑重叠区域应力分布表现为新的塑性变形导致原有的弹坑受挤压而产生变形,进而使得原有弹坑的应力松弛了68.2%,因此整体上喷丸后弹坑应力分布状况随着重叠区和凹陷区呈现波纹状起伏。研究认为,弹丸重叠撞击起到均化材料表面应力的作用。
关键词(KeyWords): 喷丸弹坑;铝合金;应力场;有限元模型;相似理论
基金项目(Foundation): 国家重点研发计划(2022YFD2202103);; 国家自然科学基金(51475483)
作者(Author): 胡俊,廖凯,罗鹏博,李立君,陈飞
DOI: 10.13289/j.issn.1009-6264.2023-0137
参考文献(References):
- [1] 熊柏青,闫宏伟,张永安,等.我国航空铝合金产业发展战略研究[J].中国工程科学,2023,25(1):88-95.XIONG Bai-qing,YAN Hong-wei,ZHANG Yong-an,et al.Development strategy for the aviation-grade aluminum alloy industry in China[J].Strategic Study of CAE,2023,25(1):88-95.
- [2] 臧金鑫,陈军洲,韩凯,等.航空铝合金研究进展与发展趋势[J].中国材料进展,2022,41(10):769-777.ZANG Jin-xin,CHEN Jun-zhou,HAN Kai,et al.Research progress and development trend of aviation aluminum alloy[J].Materials China,2022,41(10):769-777.
- [3] 刘辰辰,陈亚军,李柯,等.7075 航空铝合金原位腐蚀多轴疲劳行为分析[J].中国机械工程,2019(5):1-7.LIU Chen-chen,CHEN Ya-jun,LI Ke,et al.Analysis for in-situ corrosion-multiaxial fatigue behaviors of 7075 aerospace aluminum alloys[J].China Mechanical Engineering,2019(5):1-7.
- [4] 臧志刚,王建明,郑林彬.2024 铝合金喷丸试件疲劳寿命试验及仿真研究[J].材料保护,2018,51(5):69-73.ZANG Zhi-gang,WANG Jian-ming,ZHENG Lin-bin.Fatigue life experiment and simulation study on 2024 aluminum alloy specimen with shot peening[J].Material Protention,2018,51(5):69-73.
- [5] 高国强,陈金祥,薛红前,等.7B50-T7751铝合金喷丸强化表面形态衍化及其对疲劳性能的影响[J].中国表面工程,2022,35(4):187-195.GAO Guo-qiang,CHEN Jin-xiang,XUE Hong-qian,et al.Surface morphology evolution together with its effect on fatigue properties in shot peening of aluminum alloy 7B50-T7751[J].China Surface Engineering,2022,35(4):187-195.
- [6] 李斌,董丽虹,王海斗,等.航空航天铝合金腐蚀疲劳研究进展[J].表面技术,2021,50(7):106-118.LI Bin,DONG Li-hong,WANG Hai-dou,et al.Research progress on corrosion fatigue of aerospace aluminum alloy[J].Surface Technology,2021,50(7):106-118.
- [7] 王付胜,孔繁淇,王文平,等.航空铝合金原位腐蚀疲劳性能及断裂机理[J].材料工程,2022,50(6):149-156.WANG Fu-sheng,KONG Fan-qi,WANG Wen-ping,et al.In-situ corrosion fatigue properties and fracture mechanism of aviation aluminum alloy[J].Journal of Materials Engineering,2022,50(6):149-156.
- [8] Lv Z,Hou R G,Wang R,et al.Numerical investigation on the residual stress in abrasive waterjet peening[J].The International Journal of Advanced Manufacturing Technology,2022,123(5/6):1695-1706.
- [9] Ohta T,Ma N.Shot velocity measurement using particle image velocimetry and a numerical analysis of the residual stress in fine particle shot peening[J].Journal of Manufacturing Processes,2020,58:1138-1149.
- [10] Zhang X Z,Huang J X,Niu Z Q,et al.Analysis of shot peening residual stress distribution based on dislocation configuration[J].Materials Science and Technology,2022,38(15):1257-1265.
- [11] Wu G,Wang Z,Gan J,et al.FE analysis of shot-peening-induced residual stresses of AISI 304 stainless steel by considering mesh density and friction coefficient[J].Surface Engineering,2019,35(3):242-254.
- [12] 李开发.TC4钛合金喷丸数值模拟[D].淮南:安徽理工大学,2021.LI Kai-fa.Numerical simulation of TC4 titanium alloy shot peening[D].Huainan:Anhui University of Science and Technology,2021.
- [13] Mori K,Osakada K,Matsuoka N.Finite element analysis of peening process with plastically deforming shot[J].Journal of Materials Processing Technology,1994,45(1/4):607-612.
- [14] Meguid S A,Shagal G,Stranart J C.3D FE analysis of peening of strain-rate sensitive materials using multiple impingement model[J].International Journal of Impact Engineering,2002,27(2):119-134.
- [15] Edward A B,Heyns P S,Kok S.A numerical investigation of a single-shot in a DEM-FEM approach to shot peening simulation[J].Metals,2019,9(11):1183.
- [16] Xie L C,Wang C X,Wang L Q,et al.Numerical analysis and experimental validation on residual stress distribution of titanium matrix composite after shot peening treatment[J].Mechanics of Materials,2016,99:2-8.
- [17] Hassani-Gangaraj S M,Cho K S,Voigt H J L,et al.Experimental assessment and simulation of surface nanocrystallization by severe shot peening[J].Acta Materialia,2015,97:105-115.
- [18] 张洪伟,陈家庆,张以都.基于多丸粒模型的喷丸表面强化过程数值模拟[J].塑性工程学报,2012,19(6):118-125.ZHANG Hong-wei,CHEN Jia-qing,ZHANG Yi-du.Numerical simulation of shot-peening process based on multiple shot model[J].Journal of Plasticity Engineering,2012,19(6):118-125.
- [19] 王延忠,李菲,陈燕燕,等.TC4喷丸强化仿真与试验[J].北京航空航天大学学报,2019,45(9):1723-1731.WANG Yan-zhong,LI Fei,CHEN Yan-yan,et al.CT4 shot peening simulation and experiment[J].Journal of Beijing University of Aeronautics and Astronautics,2019,45(9):1723-1731.
- [20] 陈家伟,廖凯,车兴飞,等.铝合金喷丸应力-变形的仿真分析与实验[J].表面技术,2018,47(11):41-47.CHEN Jia-wei,LIAO Kai,CHE Xing-fei,et al.Simulation and experiment study of surface stress-deformation by shot peening on Al-based alloy[J].Surface Technology,2018,47(11):41-47.
- [21] 陈家伟,廖凯,李立君,等.铝合金喷丸工艺参数-表面特征值的函数关系与应用[J].表面技术,2019,48(6):212-220.CHEN Jia-wei,LIAO Kai,LI Li-jun,et al.Function relationship between shot peening parameters and surface characteristic of Al-based alloy and application[J].Surface Technology,2019,48(6):212-220.
- [22] Burakovsky L,Preston D L.Shear modulus at all pressures:Generalized Guinan-Steinberg formula[J].Journal of Physics & Chemistry of Solids,2006,67(9):1930-1936.
- [23] Peng J,Hu C,Li Y,et al.Determination of parameters of Steinberg-Guinan constitutive model with shock wave experiments[J].International Journal of Modern Physics B,2008,22(09n11):1111-1116.
- [24] Gao C Y,hang L,Yan H X.A new constitutive model for HCP metals[J].Materials Science and Engineering A,2011,528(13/14):4445-4452.
- [25] 杨恒,沈双全,郭聪,等.相似理论在冲击试验中的应用研究[J].核动力工程,2022,43(S1):99-102.YANG Heng,SHEN Shuang-quan,GUO Cong,et al.Application research of similarity theory in impact test[J].Nuclear Power Engineering,2022,43(S1):99-102.
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