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
机头锥蒙皮数控拉形过程全流程有限元仿真及回弹预测
英文标题:Finite element simulation and springback prediction on whole process for CNC stretch forming process of nose cone skin
作者:张贺刚1 王志成2 王晓臣2 杜建宁2 彭皓云2 朱丽2 李小强3 阳晓军4 
单位:1.航发智造(北京)科技有限公司 2.沈阳飞机工业(集团)有限公司 3.北京航空航天大学 机械工程及自动化学院 4.广州希鹏计算机科技有限公司 
关键词:蒙皮 拉形 回弹预测 数控拉形机 全流程仿真 
分类号:V260.5;TH164;TG386
出版年,卷(期):页码:2022,47(9):83-89
摘要:

 为了提高新一代飞机的气动性能,对表面外形精度的要求显著提高,因此,必须控制蒙皮拉形后的零件回弹。基于自主开发的国产蒙皮拉形仿真软件AISF,对机头锥蒙皮数控拉伸成形、切边、回弹全过程进行了有限元仿真。对VTL1000数控蒙皮拉形机的关键运动机构进行了测量,建立了考虑机床实际运动的蒙皮拉形有限元仿真模型。将实际零件数控拉形代码直接输入有限元仿真模型,保证仿真边界条件与试验完全一致。考虑实际生产条件,建立了拉形—回弹—切边—压紧仿真模型,实现了回弹的仿真预测。根据优化后的数控拉形代码,成形出了实际零件并进行了数字化检测,发现回弹预测与实际基本吻合,验证了有限元仿真模型的准确性。

 

 In order to improve the aerodynamic performance for new generation of aircraft, the requirements on the surface shape accuracy have been significantly increased, so it is necessary to control the springback of parts after the skin is stretched. Therefore, based on the self-developed domestic skin stretch forming simulation software AISF, the whole process of CNC stretch forming, trimming, springback for the nose cone skin was simulated numerically. Then, the key motion mechanism of VTL1000 CNC skin stretch forming machine was measured, and a finite element simulation model of skin stretch forming considering the actual motion of machine tool was established. Furthermore, the CNC stretch forming code of the actual parts was directly input into the finite element simulation model to ensure that the simulation boundary conditions were completely consistent with the experiment. Considering the actual production conditions, a simulation model of stretch forming-springback-trimming-pressing was established to realize the simulation prediction of springback. According to the optimized CNC stretch forming code, the actual parts were formed and digitally inspected. The results show that the springback prediction is basically consistent with the actual situation, which verifies the accuracy of the finite element simulation model.

基金项目:
国家自然科学基金面上项目(52075025)
作者简介:
张贺刚(1978-),男,硕士,工程师 E-mail:hgbox@qq.com 通信作者:李小强(1979-),男,博士,教授 E-mail:littlestrongcn@163.com
参考文献:

 [1]朱明华, 王文斌, 李小强,. 大型客机钣金数字化柔性精准成形技术[J]. 南京航空航天大学学报, 2011, 43(2):216-221.


 


Zhu M H, Wang W B, Li X Q, et al. Digital,flexible and precise forming technology of sheet metal in large airliner[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2011, 43(2):216-221.


 


[2]Corporation M S. MSC Virtual Manufacturing [R]. USA: MSC Software Corporation, 2001.


 


[3]Corporation N G. Stretch Forming Simulation (SFS) [R]. Indiana:AMSE, 1998.


 


[4]Ashbridge M T J, Leacock A G, Gilmour K R, et al. The effect of solution heat treatment and natural ageing on the yield characteristics of a 2024-O aluminium alloy[A].ASME.ASME International Mechanical Engineering Congress and Exposition[C]. USAASME, 2000.


 


[5]Leacock A G. Numerical Simulation of Anistropic Plasticity in Stretched Formed Aluminium Alloys [D]. Jordanstown: University of Ulster, 1999.


 


[6]Oding S, Stourov N. Technological Parameter Calculation and Stretch Forming Process Control of 3D Profile Parts[M]. Dordrecht: Springer Netherlands, 2003.


 


[7]Oding S S. Controlling the formation of double curvature skin elements on a program-controlled stretch former. I.[J]. Soviet Aeronautics:English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika 1987, 30(3): 57-61.


 


[8]Oding S S. Control of shaping of double-curvature skins on stretch-forming equipment with programmed control. II.[J]. Soviet Aeronautics:English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika 1987, 30(4): 44-48.


 


[9]白雪飘, 李东升, 万敏, . 基于蒙皮拉形模拟系统的数控拉形仿真与实践[J]. 塑性工程学报, 2004,11(1):43-45.


 


Bai X P, Li D S, Wan M, et al. Simulation and practice on NC stretch-forming for the stretch form system[J]. Journal of Plasticity Engineering, 2004,11(1):43-45.


 


[10]李卫东, 万敏, 韩金全. 飞机蒙皮数字化拉形系统 ASSFCAE[J]. 航空制造技术, 2007,(z1):498-503.


 


Li W D, Wan M, Han J Q. Numerical stretch forming system for aircraft skin[J]. Aeronautical Manufacturing Technology, 2007,(z1):498-503.


 


[11]李卫东, 万敏, 占强, 等.数控蒙皮横拉机运动分析与仿真控制 [J]. 北京航空航天大学学报, 2004,30(2):105-108.


 


Li W D, Wan M, Zhan Q, et al. Motion analysis and simulation control of numerical controlled transverse stretching machine for aircraft skin[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004,30(2):105-108.


 


[12]韩志仁, 孔庆猛, 孟祥韬, . 飞机蒙皮拉形加载轨迹研究[J]. 机械设计与制造, 2016,(4):258-261.


 


Han Z R, Kong Q M, Meng X T, et al. Study on loading trajectory of aircraft skin in stretch forming[J]. Machinery Design & Manufacture, 2016,(4):258-261.


 


[13]陈根发, 方继钊,王勇,等. 复杂鼓包蒙皮成形技术分析与优化[J].锻压技术,2020,45(8)82-87.


 


Chen G FFang J ZWang Yet al. Analysis and optimization on complex bulging skin forming technology[J]. Forging & Stamping Technology2020,45(8):82-87.


 


[14]房涛涛, 李晓星,郎利辉. 大厚度双曲度铝合金飞机蒙皮拉伸成形工艺优化[J]. 锻压技术,2021,46(1):29-3642.


 


Fang T TLi X XLang L H. Optimization on stretch forming process for hyperbolic aluminum alloy aircraft skin with large thickness [J]. Forging & Stamping Technology2021,46(1):29-3642.


 


 


[15]谢洪志, 王玲,赵天章,. 基于数字化的蒙皮拉形加载轨迹优化与应用[J]. 锻压技术,2021,46(1):56-59.


 


Xie H ZWang LZhao T Zet al. Optimization and application of loading trajectory in stretch forming of skin based on digital [J]. Forging & Stamping Technology2021,46(1):56-59.


 


[16]李小强, 宋楠,李东升. VTL 型数控蒙皮拉形机加载轨迹设计[J].塑性工程学报,201219 (4): 49-55.


 


Li X QSong NLi D S.Design of loading trajectory for VTL numerical control stretch forming machine[J].Journal of Plasticity Engineering201219 (4): 49-55.

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