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带下陷的直凸弯边零件回弹补偿及试验验证
英文标题:Springback compensation and experimental verification of straight convex bending parts with sagging
作者:张凌云1 徐淑赢1 李峰2 石绍秋1 尹延广1 
单位:1. 沈阳航空航天大学 2.中国人民解放军第五七二一工厂济南航空修理厂 
关键词:钣金零件 下陷 直凸弯边 橡皮囊成形 回弹补偿 
分类号:V263+2
出版年,卷(期):页码:2021,46(10):78-82
摘要:

 为提高飞机钣金零件的成形质量,对带下陷的直凸弯边零件在橡皮囊成形过程中的回弹问题进行研究。对新淬火状态下的2024-W铝合金材料进行单向拉伸试验,获得材料的力学性能参数,为回弹补偿和有限元模拟提供条件;采用CATIA二次开发系统,对带下陷的直凸弯边钣金件的圆角部分和弯边部分两个位置进行回弹补偿,生成准确的回弹补偿模具;采用Pam-stamp 2G有限元模拟软件,对新设计的补偿模具进行有限元数值模拟并进行试验验证,验证了经回弹补偿模块设计带下陷的直凸弯边补偿模具的可行性。结果表明:在成形压力为50 MPa时,零件回弹前后的角度误差为1°,满足尺寸设计要求,验证了有限元模拟的可信度以及回弹补偿系统的准确性。

 In order to improve the forming quality of aircraft sheet metal parts, the springback issue in the forming process of rubber bag for straight convex bending parts with sagging was studied. A uniaxial tensile experiment was performed on the 2024-W aluminum alloy material in the new quenched state, and the mechanical property parameters of the material were obtained, which provided conditions for springback compensation and finite element simulation. The CATIA secondary development system was used to compensate the springback in the round fillet and flanged parts of the straight convex bending sheet metal parts with sagging, and an accurate springback compensation mold was generated. The finite element simulation software Pam-stamp 2G was used to conduct numerical simulation and experimental verification for the compensation mold newly designed. The feasibility of a straight convex bending compensation mold with sagging designed by the springback compensation module was verified. The results show that when the forming pressure is 50 MPa, the angle error of part before and after springback is 1°, which meets the requirements of dimension design. The credibility of finite element simulation and the accuracy of springback compensation system are verified.

基金项目:
作者简介:
作者简介:张凌云(1963-),男,博士,教授 E-mail:zhangly79@163.com 通信作者:徐淑赢(1994-),男,硕士研究生 E-mail:1247953444@qq.com
参考文献:
[1]崔静. 钣金零件的坯料展开与回弹算法研究[D].南京:南京航空航天大学,2016.

Cui J. Research on the Algorithms of Blank Unfolding and Spring-back Simulation for Sheet Metal Parts[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016.

[2]胡丹. 飞机钛合金钣金件橡皮囊精确成形技术研究[D]. 南京:南京航空航天大学,2014.

Hu D. Precision Forming Technology Research on Rubber Bladder Forming of Aircraft Titanium Alloy Sheet Metal[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014.

[3]李文平. 弯曲回弹变分原理及其数值模拟研究[D].河北:燕山大学,2006.

Li W P. Study on Variational Principles of Springback for Bending and Its Numerical Simulation[D]. Hebei: Yanshan University, 2006.

[4]杨忆湄, 王俊彪,刘闯,等.框肋零件弯边回弹补偿系统的开发与应用[J].锻压装备与制造技术,2013,48(5):68-71.

Yang Y M, Wang J B, Liu C, et al.Development and application of flange springback compensation system for frame and rib parts[J].China Metal Forming Equipment & Manufacturing Technology,2013,48(5):68-71.

 

[5]陈磊, 邱晞,李善良,等.橡皮液压成形直弯边回弹试验与分析研究[J].塑性工程学报,2008,15(3):47-50,60.

[5]Chen L, Qiu X, Li S L,et al. Analysis and experiment study on springback of straight flanging in rubber fluid forming [J]. Journal of Plastic Engineering,2008,15 (3):47-50,60.

[6]聂昕. 汽车板件回弹相关问题的研究[D].长沙:湖南大学,2008.

Nie X. Key Teehniques Study of Automobile Pane′s Springback. [D].Changsha: Hunan University, 2008.

[7]张建明. 翼肋零件橡皮囊液压成形模具型面设计系统的研究[D].南京:南京航空航天大学,2011.

Zhang J M. Research on Die-face Design System for Rubber Bladder Hydroforming of the Rib[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011.

[8]付云方. 橡皮囊成形弯曲回弹的研究[D].南京:南京航空航天大学,2009.

Fu Y F. A Research on the Springback of Bending on Rubber Bladder Foring[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009.

[9]Subhrangshu D. The Effect of Forming Pressure on Springback in 2024 Aluminum Alloys[R]. Reno,Nevada:World Aviation Congress, 2004.

[10]张凌云, 周帅,陈瑶,等.基于补偿因子的直弯边下陷零件回弹补偿研究[J].材料科学与工艺,2018,26(4):28-33.

Zhang L Y,Zhou S,Chen Y,et al. Research on springback compensation for straight flanging jogged partbased on compensation factors[J].Materials Science and Technology,2018,26(4):28-33.

[11]HB 6470—90,飞机钣金件尺寸公差及技术条件[S].

 
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