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
非均匀网格数铣锥底瓜瓣分区滚弯成形工艺参数研究
英文标题:Research on process parameters of zoned rolling for CNC milling cone-bottomed melon petals with non-uniform mesh
作者:胡德友 李继光 杜正勇 杜佳明 王亚龙 陈凤贺 
单位:天津航天长征火箭制造有限公司 
关键词:非均匀网格 数铣锥底瓜瓣 分区滚弯成形 薄厚交界 侧轴倾斜高度差 
分类号:TG386
出版年,卷(期):页码:2020,45(9):137-142
摘要:

运载火箭箱底结构考虑到传力及空间等因素,常采用锥形底设计。针对锥形底用非均匀网格数铣锥底瓜瓣的成形精度控制,采用分区滚弯成形工艺参数进行研究,探究网格区及法兰区在成形过程中的受力变形趋势。结果表明:当数铣锥底瓜瓣受到非均匀网格的结构限制时,在网格区与焊接区的薄厚交界处存在突变,出现反向变形,相互制约;同时,发现侧轴倾斜高度差对网格区直线度的影响较小,但对于弧度间隙影响显著;由于中间网格区域与轴向上、下端辅助筋条区的强度差异,且受到网格区受力制约,轴向易呈现焊接区内凹、网格区外凸的现象,当上、下轴夹持间隙为20 mm、网格区侧轴倾斜高度差为90 mm、法兰区侧轴倾斜高度差为110 mm时,弧度间隙可控制在2.0~3.5 mm、直线度可控制在4.0~5.5 mm以内。

Considering factors such as force transmission and space, the bottom structure of launch vehicle box is often designed with cone bottom. For the control of forming accuracy on the CNC milling cone-bottomed melon petals with non-uniform mesh, the process parameters of zoned rolling were explored to investigate the force and deformation trend during the forming process in the mesh area and flange area. The results show that when the cone-bottomed melon petals with CNC milling is restricted by the non-uniform mesh structure, there is a sudden change in the boundary between thinness and thickness and the mesh area and the welding area, and the reverse deformation occurs and restricts each other. At the same time, it is found that the indination height difference of single-sided axis has a small effect on the straightness of the mesh area, but has important effects on the radian gap. Because of the difference in strength between the middle mesh area and the axial upper and lower auxiliary rib areas and the constrained forces in the mesh area, the weld area along the axial direction is concave, and the mesh area along the axial direction is convex. Furthermore, when the clamping gap between upper and lower shafts is 20 mm, the inclined height difference of single-sided axis in the mesh area and the flange area is 90 mm and 110 mm respectively, the radion gap is controlled within 2.0-3.5 mm, and the straightness is controlled within 4.0-5.5 mm.

基金项目:
天津市科技支撑项目(17YFZCGX00530)
作者简介:
胡德友(1988-),男,硕士,工程师 E-mail:hudeyou1988@126.com
参考文献:


[1]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, 2002,10(5): 17-22.


Yao J S, Zhou W S, Wang G Q,et al.The development of materials and welding technology of the tank
[J]. Aerospace Manufacturing Technology, 2002, 10(5): 17-22.



[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]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.



[4]曾元松, 黄遐. 大型整体壁板成形技术
[J]. 航空学报,2008,(3): 721- 727.


Zeng Y S, Huang X. Forming technologies of large integral panel
[J]. Acta Aeronautica et Astronautica Sinica, 2008,(3): 721-727.



[5]Wang T, Platts M J, Wu J. The optimisation of shot peen forming processes
[J]. Journal of Materials Processing Technology, 2008,206(1-3): 78-82.



[6]黄晓婧, 王俊彪,张贤杰. 铝合金时效蠕变与时效应力松弛关系研究
[J]. 航空制造技术, 2011,(11): 99-101.


Huang X J, Wang J B, Zhang X J. Research on relationship between aging creep and stress relaxation Al-alloy
[J]. Aeronautical Manufacturing Technology,2011,(11): 99-101.



[7]Wan M,Yang Y Y,Li S B. Determination of the limiting drawing coefficient in the deep drawing of conical cups
[J].Journal of Materials Processing Technology,2001,114 (2): 114-117.



[8]陈齐广. 圆锥形件拉深成形侧壁起皱预测
[D].湘潭: 湘潭大学,2015.


Chen Q G.Prediction of Wall Wrinkling in Deep Drawing of Conical Parts
[D].Xiangtan: Xiangtan University,2015.



[9]夏琴香, 阮锋,岛进,等. 锥形件柔性旋压成形时的变形力分析
[J]. 金属成形工艺,2002,20(3):5-8.


Xia Q X, Ruan F, Shima S, et al.Analysis of the spinning forces on flexible spinning of cones
[J]. Metal Forming Technology, 2002,20(3):5-8.



[10]赵小凯, 徐文臣,陈宇,等.TA15钛合金筒-锥复合曲母线构件旋压成形工艺研究
[J].材料科学与工艺,2016,24(4): 10-17.


Zhao X K,Xu W C,Chen Y,et al. Study on the spinning process of cylinder-conical composite curved generatrix workpiece of TA15 titanium alloy
[J]. Materials Science and Technology,2016,24(4): 10-17.



[11]Sekiguchi A,Arai H.Control of wall thickness distribution by oblique shear spinning methods
[J].Journal of Materials Processing Technology,2012,212 (4): 786-793.



[12]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.



[13]余同希, 章亮炽.塑性弯曲理论及其应用
[M]. 北京: 科学出版社,1992.


Yu T X,Zhang L Z.Plastic Bending Theory and Its Application
[M]. Beijing: Science Press,1992.



[14]李建, 陈举庆,姚久军. 四辊卷板机弯卷工艺及辊位移计算模型
[J]. 一重技术,2015,(3):1-5.

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