7085铝合金残余应力及加工变形的数值仿真与试验

doi:10.7527/S1000-6893.2013.0469

材料工程与机械制造

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7085铝合金残余应力及加工变形的数值仿真与试验

杨吟飞, 张峥, 李亮, 何宁, 赵威

南京航空航天大学机电学院, 江苏南京 210016

收稿日期:2013-09-05 修回日期:2013-11-16 出版日期:2014-02-25 发布日期:2013-11-20
通讯作者: 杨吟飞，Tel.：025-84892502 E-mail：yyfgoat@nuaa.edu.cn E-mail:yyfgoat@nuaa.edu.cn
作者简介:杨吟飞男，博士后，讲师。主要研究方向：航空结构件加工变形分析。Tel：025-84892502 E-mail：yyfgoat@nuaa.edu.cn；张峥男，博士研究生。主要研究方向：航空结构件加工变形分析。Tel：025-84892502 E-mail：zhangzheng@nuaa.edu.cn；李亮男，博士，教授，博士生导师。主要研究方向：高速、高效切削加工、微细铣削技术、切削加工变形分析与控制。Tel：025-84896040 E-mail：liliang@nuaa.edu.cn
基金资助:
国防技术基础科研项目（C1520120002，J1520130001）；高等学校博士学科点专项科研基金（20123218120025）；中央高校基本科研业务费专项资金（NS2012011）

Numerical Simulation and Test of Bulk Residual Stress and Machining Distortion in Aluminum Alloy 7085

YANG Yinfei, ZHANG Zheng, LI Liang, HE Ning, ZHAO Wei

College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received:2013-09-05 Revised:2013-11-16 Online:2014-02-25 Published:2013-11-20
Supported by:
Defense Industrial Technology Development Program (C1520120002, J1520130001); Research Fund for the Doctoral Program of Higher Education of China (20123218120025); The Fundamental Research Funds for the Central Universities (NS2012011)

摘要/Abstract

摘要：

毛坯残余应力的测量以及零件的加工变形分析是航空整体结构件数控加工工艺研究的难题。应用MSC.Marc软件对某型飞机主起支撑接头的7085铝合金锻件毛坯的淬火-压缩工艺进行了数值仿真，获得了毛坯残余应力分布趋势；应用X射线衍射法与钻孔法测量了毛坯表层残余应力分布，提出了基于系数修正法的毛坯残余应力分析方法，通过最小二乘法（LSM）拟合仿真值与试验值以获得应力修正系数，并对毛坯残余应力分布的仿真结果进行修正，获得了实际毛坯的残余应力分布；由此进行了主起支撑接头缩比零件加工变形仿真与验证试验。研究结果表明：7085铝合金块状毛坯残余应力数值仿真结果与测试结果的趋势吻合，为应力修正提供了物理基础；相对于未修正的应力分布，基于修正后的应力分布仿真获得的变形结果精度提高了50%；7085-T7452铝合金的毛坯残余应力是导致主起支撑接头加工变形的主要因素。

关键词: 残余应力, 加工变形, X射线衍射, 钻孔法, 系数修正

Abstract:

Bulk residual stress and machining distortion of aluminum parts are major concerns in the manufacturing of aerospace monolithic components. The quenching and cold compression residual stresses of main support device for landing gear made from aluminum alloy 7085 are simulated using MSC.Marc software. The surface residual stress of specimen is measured using both X-ray diffraction and hole drilling method. By comprising residual stress between simulation and measurement, residual stress simulation is corrected using least squares method (LSM). Then the machining distortion simulation and experiment are carried out on scaled part based on the coefficient corrected residual stress. The results indicate that the stress distribution tendencies in specimen are quite similar between simulation and measurement; X-ray diffraction and hole drilling method results are found in a good agreement with each other; the analytical accuracy based on the corrected residual stress using LSM is enhanced by about 50% on predicting machining distortion. Machining distortion can be mainly attributed to bulk residual stress within material.

Key words: residual stresses, machining distortion, X-ray diffraction, hole drilling method, coefficient modification

中图分类号:

杨吟飞, 张峥, 李亮, 何宁, 赵威. 7085铝合金残余应力及加工变形的数值仿真与试验[J]. 航空学报, 2014, 35(2): 574-581.

YANG Yinfei, ZHANG Zheng, LI Liang, HE Ning, ZHAO Wei. Numerical Simulation and Test of Bulk Residual Stress and Machining Distortion in Aluminum Alloy 7085[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(2): 574-581.

参考文献

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E-mail：hkxb@buaa.edu.cn

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7085铝合金残余应力及加工变形的数值仿真与试验

Numerical Simulation and Test of Bulk Residual Stress and Machining Distortion in Aluminum Alloy 7085

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