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Title:Influence of auxiliary rib thickness on forming accuracy for CNC milling short shell panel of 2219 ceramic-aluminum material
Authors: Li Jiguang Hu Deyou Wang Yalong Du Baihong Zhao Yanguang Chen Zhe 
Unit: Tianjin Long March Launch Vehicle Manufacturing Co. Ltd. Shanghai Jiao Tong University 
KeyWords: 2219 ceramic-aluminum material  CNC milling short shell panel  pressing amount auxiliary ribs relative bending radius 
ClassificationCode:TG386
year,vol(issue):pagenumber:2021,46(7):60-65
Abstract:
Taking the CNC milling short shell panel of 2219 ceramic-aluminum material in the launch vehicle tank as research object,through the analysis of product structure characteristics, the boss and grid areas were partitioned and formed by four-axis roll bending method, and the clamping gap of upper and lower shafts and the pressing amount were reasonably controlled. Then, the influence mechanism for the thickness of auxiliary ribs at the upper and lower ends of heading on the forming process parameters and the profile accuracy was explored to realize the engineering application of 2219 ceramic-aluminum material. The results show that the plastic flow of materials and the relative bending radius are influenced by the thickness of auxiliary ribs under the same radius of module curvature, and the forming process parameters and the product accuracy are restricted by three-dimensional stress in bending. In addition, when the thickness of auxiliary ribs is 6 mm, it produces a larger proportion of plastic deformation than that when the thickness is 5 mm, and it is easier to meet the requirements of forming curvature, which has a significant impact, but it has little effect on the arc forming accuracy. Finally, when there are three auxiliary ribs with the thickness of 5 mm at the upper and lower ends of heading for the CNC milling short shell panel, the arc gap clearance, the straightness of welding zone and the straightness of grid area are controlled within 2, 1.5 and 2.5 mm, respectively.
Funds:
天津市科技支撑项目(17YFZCGX00530)
AuthorIntro:
作者简介:李继光(1981-),男,博士,高级工程师,E-mail:jiguangli2008@126.com
Reference:
[1]刘欣, 王国庆,李曙光,等. 重型运载火箭关键制造技术发展展望[J]. 航天制造技术,2013,(1):1-6.
Liu X,Wang G Q,Li S G,et al. Forecasts on crucial manufacturing technology development of heavy lift launch vehicle[J]. Aerospace Manufacturing Technology,2013(1):1-6.
[2]龙乐豪, 李平岐, 秦旭东,等. 我国航天运输系统60年发展回顾[J].宇航总体技术,2018,2(2):1-6.
Long L H, Li P Q, Qin X D,et al.The review on China space transportation system of past 60 years[J]. Astronautical Systems Engineering Technology, 2018, 2(2): 1-6.
[3]姚君山, 周万盛,王国庆,等. 航天贮箱结构材料及其焊接技术的发展[J]. 航天制造技术, 2002,(5): 17-22.
Yao J S, Zhou W S, Wang G Q,et al.The development structure of materials and their welding technology of space vehicle propellant tanks[J]. Aerospace Manufacturing Technology, 2002,(5): 17-22.
[4]Dinaharan I, Murugan N. Effect of friction stir welding on microstructure,mechanical and wear properties of AA6061/ZrB2 in situcast composites[J].Materials Science and Engineering: A,2012,543: 257-266.
[5]张荻, 张国定,李志强.金属基复合材料的现状与发展趋势[J]. 中国材料进展,2010,29(4): 1-7.
Zhang D, Zhang G D, Li Z Q. The current state and trend of metal matrix composites[J]. Materials China,2010,29(4): 1-7.
[6]Schaffer P L,Miller D N,Dahle A K. Crystallography of engulfed and pushed TiB2 particles in aluminium[J]. Scripta Materialia,2007,57(12): 1129-1132.
[7]于登云, 赖松柏,陈同祥.大型空间站整体壁板结构技术进展[J].中国空间科学技术,2011,31 (5): 31-40.
Yu D Y,Lai S B,Chen T X.Review on integral stiffened shell structure technology of large space station [J]. Chinese Space Science and Technology,2011,31 (5): 31-40.
[8]赖松柏, 陈同祥,于登云.整体壁板填料辅助滚弯成形的动力显式分析方法[J]. 航天器工程,2012,21 (3): 41-47.
Lai S B,Chen T X,Yu D Y. Dynamic explicit analysis method for roll bending forming of integrally stiffened panel with rubber filler[J]. Spacecraft Engineering,2012,21 (3): 41-47.
[9]韩志仁, 戴良景,张凌云. 飞机大型蒙皮和壁板制造技术现状综述[J]. 航空制造技术,2009,(4): 64- 66.
Han Z R, Dai L J, Zhang L Y. Current status of large aircraft skin and panel manufacturing technologies[J].Aeronautical Manufacturing Technology, 2009,(4):64-66.
[10]刘劲松, 张士宏, 曾元松,等. 网格式整体壁板增量成形有限元模拟[J] . 材料科学与工艺, 2004,12(5): 515-517
Liu J S,Zhang S H,Zeng Y S,et al. Simulation of incremental forming on integral panel skin with grid-type ribs [J]. Materials Science & Technology,2004,12 (5): 515-517.
[11]胡德友, 李继光,朱亚蓉,等.单侧轴倾斜角度对小锥角锥度壁板成形精度的影响[J] 锻压技术,2020,45(6): 59-63.
Hu D Y,Li J G,Zhu Y R,et al.Influence of the inclination angel of single-axis on the forming precision of the panel with small taper [J]. Forging & Stamping Technology,2020,45(6): 59-63.
[12]王艳, 朱新庆,胡捷飞,等.四辊卷板机连续滚弯成形工艺的数值模拟研究[J]. 系统仿真学报,2018,30(5):1772-1780.
Wang Y, Zhu X Q, Hu J F, et al. Research on numerical simulation of continuous roll forming process of four-roll plate bending machines[J]. Journal of System Simulation,2018,30(5): 1772-1780.
[13]余同希. 塑性弯曲理论及其应用[M]. 北京: 科学出版社,1992.
Yu T X. Plastic Bending Theory and Its Application[M]. Beijing: Science Press,1992.
[14]俞汉清, 陈金德. 金属塑性成形原理[M]. 北京: 机械工业出版社, 1999.
Yu H Q, Chen J D. Fundamental of Metal Plastic Forming[M]. Beijing: China Machine Press, 1999.
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