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铝锂合金喷丸强化数值模拟及试验
引用本文:王永军,孙宝龙,张炜,高国强,乔明杰.铝锂合金喷丸强化数值模拟及试验[J].航空动力学报,2015,30(3):595-602.
作者姓名:王永军  孙宝龙  张炜  高国强  乔明杰
作者单位:1. 西北工业大学机电学院,西安,710072
2. 中国航空工业集团公司中航飞机股份有限公司西安飞机分公司,西安,710089
基金项目:国家自然科学基金(51275420)
摘    要:根据喷丸强化工艺过程的特点,利用ABAQUS有限元计算软件建立了模拟喷丸残余应力场的三维有限元模型.在此模型基础上研究了喷丸速度、弹丸直径及弹丸数量等因素对铝锂合金喷丸残余应力场的影响规律,进而对比了单弹丸模型、均布式阵列弹丸模型和随机弹丸模型下残余应力场的分布规律.采用X射线残余应力仪和电解抛光法得到喷丸强化后沿铝锂合金试件厚度方向的残余应力分布规律.残余应力层深度约为0.24mm,最大残余应力出现在距表面深度为0.08mm处,验证了有限元模型的有效性.

关 键 词:铝锂合金  喷丸强化  有限元模拟  残余应力  弹丸模型
收稿时间:2013/10/28 0:00:00

Numerical simulation and experiment on shot peening of Al-Li alloy
WANG Yong-jun,SUN Bao-long,ZHANG-Wei,GAO Guo-qiang and QIAO Ming-jie.Numerical simulation and experiment on shot peening of Al-Li alloy[J].Journal of Aerospace Power,2015,30(3):595-602.
Authors:WANG Yong-jun  SUN Bao-long  ZHANG-Wei  GAO Guo-qiang and QIAO Ming-jie
Institution:School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072,School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072,Xi'an Aircraft Industry Company, Aircraft Company Limited, Aviation Industry Corporation of China, Xi'an 710089, China,Xi'an Aircraft Industry Company, Aircraft Company Limited, Aviation Industry Corporation of China, Xi'an 710089, China and Xi'an Aircraft Industry Company, Aircraft Company Limited, Aviation Industry Corporation of China, Xi'an 710089, China
Abstract:According to the characteristics of shot peening process, a three-dimensional finite element model was established by using ABAQUS finite element software to simulate the residual stress field. Based on this model, the effects of shot parameters such as velocity, diameter and shot number on residual stress field of Al-Li alloy were studied respectively. Then the distributions of the residual stress field of single shot model, uniform array shots model and random shot model were compared. Furthermore, the residual stress distribution in Al-Li alloy specimen thickness direction was measured by using X-ray residual stress analyzer and electrolytic polishing method. The depth of residual stress layer is 0.24mm. The maximum residual stress occurs at the depth of 0.08mm. It verifies the validity of the finite element model.
Keywords:Al-Li alloy  shot peening  finite element simulation  residual stress  shot model
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