锻压技术

2A16铝合金簸箕形薄壁件成形工艺

英文标题：Forming process on dustpan-shaped thin-wall part for 2A16 aluminum alloy

作者：车利郭全庆刘波李小曼董东岳

分类号：TG386

出版年,卷(期):页码：2022,47(12):87-93

摘要：

确定了一种2A16铝合金簸箕形薄壁件的成形工艺方案，并采用DYNAFORM软件进行有限元模拟，研究成形过程中的裂纹和起皱等影响产品质量的问题。通过模拟分析得到了铝合金簸箕形薄壁件在不同凸凹模间隙和压边力下的凸凹模间隙-最大减薄率和增厚率曲线、压边力-最大减薄率曲线、压边力-最大增厚率曲线，对比了不同毛坯尺寸时的工件成形质量，确定了最佳工艺参数为：毛坯尺寸为237.42 mm×319.24 mm、凸凹模间隙为1.75 mm、压边力为50 kN。将成对拉深与单件拉深进行对比，发现材料利用率提升了48.498%，产品加工效率提高了1倍。最终通过拉深成形实验，验证了成对拉深成形方案和各工艺参数的合理性，为簸箕形薄壁件的成形提供了技术参考。

A forming process scheme of dustpan-shaped thin-walled part for 2A16 aluminum alloy was determined, and software DYNAFORM was used for finite element simulation to study the problems affecting the product quality such as cracks and wrinkles during the forming process. Then, for aluminum alloy dustpan-shaped thin-walled part, the punch-die clearance-maximum thinning rate and thickening rate curves blank holder force-maximum thinning rate curve, and blank holder force-maximum thickening rate curve were obtained by simulation analysis at different punch-die clearances and blank holder forces, and by comparing the forming quality of workpiece with different blank sizes, the optimal process parameters were determined as the blank size of 237.42 mm×319.24 mm, the punch-die clearance of 1.75 mm and the blank holder force of 50 kN. Furthermore, compared with single piece deep drawing, the material utilization rate was increased by 48.498%, and the product processing efficiency was doubled by paired deep drawing. Finally, through the deep drawing experiment, the rationality of the paired deep drawing scheme and the process parameters were verified, which provided technical reference for the forming of dustpan-shaped thin-wall parts.

基金项目：

车利（1990-），男，学士，工程师 E-mail：1025945001@qq.com

参考文献：

[1]Cole G S，Sherman A M. Light weight materials for automotive applications [J]. Materials Characterization,1995,35(1):3-9.

[2]杨希英,郎利辉,郭禅,等. 2A16铝合金锥形件多级充液热成形仿真及优化分析[J]. 精密成形工程,2014,6(6):72-77.

Yang X Y, Lang L H, Guo C, et al. Simulation and optimization analysis of multistage liquid filling hot forming of 2A16 aluminum alloy conical parts [J]. Journal of Netshape Forming Engineering,2014,6(6):72-77.

[3]邓鹏辉，张世兴. 固溶处理对2A16铝合金显微组织和性能的影响[J]. 装备制造技术,2009,(9):36-38.

Deng P H, Zhang S X. Effect of solution treatment on microstructure and properties of 2A16 aluminum alloy [J]. Equipment Manufacturing Technology,2009,(9):36-38.

[4]Starke E A，Staley J T. Application of modern aluminum alloys to aircraft [J]. Progress in Aerospace Sciences,1996，32（2-3）:131-172.

[5]Heinz A，Haszler A，Keidel C，et al. Recent development in aluminium alloys for aerospace application [J].Materials Science and Engineering A, 2000，280（1）:102-107.

[6]Belov N A, Alabin A N，Matveeva I A.Optimiation of phase composition of Al-Cu-Mn-Zr-Sc alloys for rolled products without requirement for solution treatment and quenching [J].Journal of Alloys and Compounds, 2014,583:206-213.

[7]Malarvizhi S, Balasubramanian V.Effect of welding processes on AA2219 aluminum joint properties [J]. Transactions of Nonferrous Metals Society of China,2011,21(5):962-973.

[8]刘兵，彭超群，王日初，等.大飞机用铝合金的研究现状及展望[J]. 中国有色金属学报，2010,20(9):1705-1715.

Liu B, Peng C Q, Wang R C, et al. Research status and prospect of aluminum alloy for large aircraft [J].The Chinese Journal of Nonferrous Metals, 2010,20(9):1705-1715.

[9]任丽萍. 高强韧铸造铝合金组织与性能研究[D]. 太原：中北大学，2014.

Ren L P. Study on Microstructure and Properties of High Strength and Toughness Cast Aluminum Alloy [D]. Taiyuan: North University of China, 2014.

[10]龚习，王恒强，付敏敏，等. 航空航天用Al-Cu-Mn系高强铝合金的研究进展[J].热加工工艺,2015,44(22):6-10.

Gong X, Wang H Q, Fu M M, et al. Research progress of Al-Cu-Mn high strength aluminum alloys for aerospace applications[J].Hot Working Technology,2015,44(22):6-10.

[11]张喆，洪润洲，周永江，等. 高强铝合金薄壁件熔铸工艺[J]. 热加工工艺,2013,42(9):78-80.

Zhang Z, Hong R Z, Zhou Y J, et al. Melting and casting process of high strength aluminum alloy thin-walled parts [J].Hot Working Technology,2013,42(9):78-80.

[12]何移峰. LY16铝合金抛物线曲面薄壁零件充液拉深成形工艺研究[D]. 哈尔滨：哈尔滨工业大学,2017.

He Y F. Study on Liquid Filled Deep Drawing Process of LY16 Aluminum Alloy Thin-wall Parts with Parabolic Curved Surface [D]. Harbin: Harbin Institute of Technology,2017.

[13]王燕齐.6061铝合金板材冲压性能与伺服成形工艺研究[D].广州：广东工业大学,2019.

Wang Y Q. Research on Stamping Performance and Servo Forming Process of 6061 Aluminum Alloy Sheet [D]. Guangzhou: Guangdong University of Technology,2019.

[14]王凤琴,赵军,官英平.毛坯外形对盒形件拉深成形的影响[J].中国机械工程,2003,14(7):619-622.

Wang F Q, Zhao J, Guan Y P. Effect of blank shape on deep drawing of box parts [J]. Chinese Journal of Mechanical Engineering,2003,14(7):619-622.

[15]郝美刚.方盒形件拉深压边力与摩擦的数值模拟研究[D]. 哈尔滨：哈尔滨工程大学,2011.

Hao M G. Numerical Simulation of Blank Holder Force and Friction in Square Box Drawing [D]. Harbin: Harbin Engineering University,2011.

[16]薛敞翔.冲压模具设计制造难点与窍门[D].北京:机械工业出版社,2003.

Xue C X. Difficulties and Tips of Stamping Die Design and Manufacturing [D]. Beijing: China Machine Press,2003.

[17]石美华.薄壁盒形件法兰区起皱影响因素的有限元模拟研究[J].现代制造工程, 2013, 6(1):91-95.

Shi M H. Finite element simulation study on influence factors of flange wrinkling in thin-walled box parts [J]. Modern Manufacturing Engineering, 2013, 6(1):91-95.

[18]陈珏.高强钢矩形件拉深成形的数值模拟研究[D].天津：天津科技大学,2013.

Chen J. Numerical Simulation Research on Deep Drawing of High Strength Steel Rectangular Parts [D]. Tianjin: Tianjin University of Science and Technology,2013.

服务与反馈：

【文章下载】【加入收藏】