网站首页期刊简介编委会过刊目录投稿指南广告合作征订与发行联系我们English
7B04铝合金带筋构件的蠕变时效变形行为研究
英文标题:Research on deformation behavior of creep age forming for 7B04 aluminum alloy stiffened components
作者:吕凤工 黄遐 曾元松 
单位:北京航空制造工程研究所 
关键词:7B04铝合金 蠕变时效成形 回弹率 数值模拟 
分类号:TG306
出版年,卷(期):页码:2015,40(3):99-103
摘要:

为研究弹性预加载范围内7B04T651铝合金带筋构件的蠕变时效变形规律,进行了140 ℃/20 h的蠕变时效成形试验,分析弯曲半径、蒙皮厚度、筋条宽度和筋条高度对回弹率的影响。同时,运用建立的蠕变本构方程和有限元分析模型对蠕变时效成形过程进行仿真分析,计算得到不同条件下的回弹率。结果表明:蒙皮越厚、筋条越高,则回弹率越低;弯曲半径越大、筋条越宽,则回弹率越高。弯曲半径和筋条高度是影响回弹率的主要因素,有限元计算回弹率与试验结果吻合较好,验证了有限元分析模型的准确性。

For the study on the deformation regularity of creep age forming of 7B04T651 aluminium component with stiffeners under elastic preloading, the experiments of creep age forming were operated at 140 ℃/20 h. And the influences of the curvature radius, skin thickness, stiffener width and stiffener height on the component springback rate were analyzed. At the same time, the constitutive equation and finite element model were established, and the forming process was simulated. After that, the springback rates under different conditions were computed. The results show that the springback rate decreases when the skin thickness and the stiffener height increase. The springback rate increases when the curvature radius and the stiffener width increase. The main factors which impact the springback rate are the curvature radius and the stiffener height. The springback rates of experiments are in accordance with that of numerical results, and the correctness of the finite element model is verified.
 

基金项目:
国家自然科学基金资助项目(50975267)
作者简介:
吕凤工(1988-),男,硕士,助理工程师
参考文献:


[1]Holman M C. Autoclave age forming large aluminum aircraft panels [J]. Journal of Mechanical Working Technology, 1989, 20: 477-488.
[2]曾元松, 黄遐, 黄硕. 蠕变时效成形技术研究现状与发展趋势[J]. 塑性工程学报, 2008, 15(3): 1-8.Zeng Y S, Huang X, Huang S. The research situation and the developing tendency of creep age forming technology [J]. Journal of Plasticity Engineering, 2008, 15(3): 1-8.
[3]Zhan L H, Lin J G, Dean T A. A review of the development of creep age forming: Experiment, modeling and applications [J]. International Journal of Machine Tools & Manufacture, 2011, 51(1): 1-17.成形有限元分析[J]. 南昌航空大学学报, 2012, 26(1): 28-34.Liu D H, Li J C, Xiong H M. Finite element analysis on creep age forming of the welded rib-web panels of 2A12 aluminum alloy [J]. Journal of Nanchang Hangkong University: Natural Sciences, 2012, 26(1): 28-34.
[6]贾树峰, 湛利华, 徐晓龙. 带筋铝合金壁板蠕变时效成形回弹行为试验[J]. 塑性工程学报, 2013, 20(1): 80-83.Jia S F, Zhan L H, Xu X L. Experimental research on the springback in creep age forming of aluminum alloy panel with stiffeners[J]. Journal of Plasticity Engineering, 2013, 20(1): 80-83.
[7]湛利华, 徐晓龙, 贾树峰,等. 7055铝合金加筋板蠕变时效成形有限元仿真[J]. 中国有色金属学报, 2013, 23(8): 2104-2109.Zhan L H, Xu X L, Jia S F, et al. Finite element simulation for creep age forming of 7055 aluminum alloy stiffened panel[J]. The Chinese Journal of Nonferrous Metals, 2013, 23(8): 2104-2109.
[8]Kowalewski Z L, Hayhurst D R, Dyson B F. Mechanisms-based creep constitutive equations for an aluminum alloy [J]. Journal of Strain Analysis, 1994, 29(4): 309-316.
[9]Huang L, Wan M, CHI C L, et al. FEM analysis of springback in age forming for aluminum alloy plate[J]. Chinese Journal of Aeronautics, 2007, 20(6): 564-569.
[10]吕凤工, 黄遐, 曾元松, 等. 7050铝合金蠕变时效成形本构模型研究[J]. 材料科学与工艺, 2014, 22(3): 28-33.Lv F G, Huang X, Zeng Y S, et al. Research on constitutive model of 7050 aluminum alloy for creep age forming [J]. Materials Science & Technology, 2014, 22(3): 28-33.
[11]李超, 万敏, 金兴, 等. 7B04铝合金蠕变时效成形本构模型研究与有限元应用[J]. 塑性工程学报, 2010, 17(5): 61-65.Li C, Wan M, Jin X, et al. A creep forming constitutive model of 7B04 aluminum alloy and its application in FEM [J]. Journal of Mechanical Working Technology, 2010, 17(5): 61-65.

服务与反馈:
文章下载】【加入收藏
《锻压技术》编辑部版权所有

中国机械工业联合会主管  中国机械总院集团北京机电研究所有限公司 中国机械工程学会主办
联系地址:北京市海淀区学清路18号 邮编:100083
电话:+86-010-82415085 传真:+86-010-62920652
E-mail: fst@263.net(稿件) dyjsjournal@163.com(广告)
京ICP备07007000号-9