2195铝锂合金薄壁网格筋筒段旋压成形工艺分析

孟佳杰, 徐晨, 涂宇杰, 石文展, 王玮, 周贤军, 于忠奇, 彭赫力

精密成形工程 ›› 2025, Vol. 17 ›› Issue (12) : 95-103.

PDF(2652 KB)
PDF(2652 KB)
精密成形工程 ›› 2025, Vol. 17 ›› Issue (12) : 95-103. DOI: 10.3969/j.issn.1674-6457.2025.12.010
航天先进制造技术

2195铝锂合金薄壁网格筋筒段旋压成形工艺分析

  • 孟佳杰1, 徐晨1, 涂宇杰1, 石文展1, 王玮1, 周贤军1, 于忠奇2, 彭赫力1,*
作者信息 +

Analysis of Spinning Forming Process for Thin-walled Cylinders with Cross Ribs of 2195 Aluminum-lithium Alloy

  • MENG Jiajie1, XU Chen1, TU Yujie1, SHI Wenzhan1, WANG Wei1, ZHOU Xianjun1, YU Zhongqi2, PENG Heli1,*
Author information +
文章历史 +

摘要

目的 针对2195铝锂合金薄壁网格筋筒段旋压成形过程中存在的流动性不足、薄壁网格筋筒段筋条部位材料填充不充分、最终影响筒段综合性能的问题,分析旋压过程中关键工艺参数对2195铝锂合金薄壁网格筋筒段筋条填充的影响。方法 基于有限元模拟仿真的方法分析了旋压过程中的关键工艺参数,选取筒段典型筋条特征截面位置展开分析,以旋压成形后筋条的高度作为成形后网格筋筒段筋条填充饱满程度的指标,分析了旋压温度、进给比、旋轮径向错距量分配方式3种工艺参数对2195铝锂合金薄壁网格筋筒段筋条填充饱满程度的影响。结果 仿真结果表明,相对的旋压温度对网格筋筒段筋条填充饱满度影响并不大,但适当升温有利于降低材料弹性模量、强度和结构刚性,从而实现旋压后回弹的降低,提高材料贴模度,提高成形精度;随着旋压进给比的增加,网格筋筒段的筋条填充性先升后降,当旋压进给比为2~4 mm/r时,筋条填充性能较好;对于径向错距量,当采用平均分配方式时,有利于筋条填充。结论 当采用本文仿真分析获得的工艺参数时,旋压成形出具有较高尺寸精度、直径200 mm及550 mm的2195铝锂合金网格筋筒段缩比样件及全尺寸样件。

Abstract

The work aims to analyze the effect of key process parameters of spinning forming on the rib filling fullness of 2195 aluminum-lithium (Al-Li) alloy to solve the problem that it is difficult to achieve sufficient material filling in the ribs during the spinning forming of thin-walled cylinders with cross ribs of 2195 Al-Li alloy due to insufficient material flowability, which affects the overall performance of cylinders. Based on the finite element simulation method, key process parameters of spinning forming were analyzed from the characteristic cross-sectional positions of typical ribs in cylinders. Taking the rib height after spinning forming as the indicator of the filling fullness of ribs in cylinders of cross ribs after forming, the influences of three process parameters, namely spinning temperature, feed ratio, and the distribution method of radial offset of the spinning wheel, on the fullness of thin-walled cylinders with cross ribs of 2195 Al-Li alloy were analyzed. The results show that the spinning temperature had little influence on the ribs height. However, increasing the temperature was beneficial to reducing the elastic modulus, strength and structural rigidity of the material, decreasing the springback after spinning and improving the fittability and forming precision. With the increase of the spinning feed ratio, the rib filling fullness first increased and then decreased. When the spinning feed ratio was in the range of 2-4 mm/r, the rib filling fullness was better. It was beneficial for rib filling fullness to adopt the average distribution method for the stepped amount of the radial. Based on the process parameters obtained from the simulation analysis in this paper, scaled and full-scale samples of thin-walled cylinder with cross ribs of 2195 Al-Li alloy with diameters of 200 mm and 550 mm and high dimensional accuracy are formed.

关键词

2195铝锂合金 / 薄壁网格筋筒段 / 流动旋压 / 筋条填充饱满度 / 有限元仿真

Key words

2195 Al-Li alloy / thin-walled cylinders with cross ribs / flow spinning forming / rib filling fullness / finite element simulation

引用本文

导出引用
孟佳杰, 徐晨, 涂宇杰, 石文展, 王玮, 周贤军, 于忠奇, 彭赫力. 2195铝锂合金薄壁网格筋筒段旋压成形工艺分析[J]. 精密成形工程. 2025, 17(12): 95-103 https://doi.org/10.3969/j.issn.1674-6457.2025.12.010
MENG Jiajie, XU Chen, TU Yujie, SHI Wenzhan, WANG Wei, ZHOU Xianjun, YU Zhongqi, PENG Heli. Analysis of Spinning Forming Process for Thin-walled Cylinders with Cross Ribs of 2195 Aluminum-lithium Alloy[J]. Journal of Netshape Forming Engineering. 2025, 17(12): 95-103 https://doi.org/10.3969/j.issn.1674-6457.2025.12.010
中图分类号: TG306   

参考文献

[1] PRASAD N E, GOKHALE A A, RAO P R.Aluminum-Lithium Alloys: Processing, Properties, and Applications[M]. Amsterdam: Elsevier, 2014: 221-249.
[2] 廖文和, 戴宁. 航空航天结构轻量化设计制造技术发展现状与挑战[J]. 南京航空航天大学学报, 2023, 55(3): 347-360.
LIAO W H, DAI N.Development and Challenge of Lightweight Design and Manufacturing Technology for Aerospace Structures[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2023, 55(3): 347-360.
[3] 张卫红, 唐长红. 航空航天装备的轻量化: 挑战与未来[J]. 航空学报, 2024, 45(5): 529965.
ZHANG W H, TANG C H.Lightweighting of Aerospace and Aeronautical Equipment: Challenges and Perspectives[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529965.
[4] 黄晓敏, 管奔, 臧勇. 航空铝锂合金热成形研究进展[J]. 稀有金属材料与工程, 2022, 51(12): 4745-4756.
HUANG X M, GUAN B, ZANG Y.Research Process on Thermal Formability of Al-Li Alloys for Aeronautic Industry[J]. Rare Metal Materials and Engineering, 2022, 51(12): 4745-4756.
[5] RIOJA R J, LIU J.The Evolution of Al-Li Base Products for Aerospace and Space Applications[J]. Metallurgical and Materials Transactions A, 2012, 43(9): 3325-3337.
[6] 刘志鹏, 肖阳, 马凯杰, 等. 航空航天铝锂合金开发及其研究进展[J]. 材料热处理学报, 2023, 44(11): 8-17.
LIU Z P, XIAO Y, MA K J, et al.Development and Research Progress of Aerospace Al-Li Alloys[J]. Transactions of Materials and Heat Treatment, 2023, 44(11): 8-17.
[7] SAJI S, HORI S.Mechanical Properties of Aluminum Alloy at very Low Temperature[J]. Journal of Japan Institute of Light Metals, 1989, 39(8): 574-583.
[8] 吴秀亮, 刘铭, 臧金鑫, 等. 铝锂合金研究进展和航空航天应用[J]. 材料导报, 2016, 30(S2): 571-578.
WU X L, LIU M, ZANG J X, et al.Research Progress and Aerospace Application of Al-Li Alloy[J]. Materials Reports, 2016, 30(S2): 571-578.
[9] DURSUN T, SOUTIS C.Recent Developments in Advanced Aircraft Aluminium Alloys[J]. Materials & Design (1980-2015), 2014, 56: 862-871.
[10] 邓名洋, 李瑞金, 王硕, 等. 铝锂合金热处理工艺及其对材料性能影响研究现状[J]. 有色金属加工, 2023, 52(4): 17-25.
DENG M Y, LI R J, WANG S, et al.Study on Heat Treatment Process and Its Effect on Material Properties of Al-Li Alloy[J]. Nonferrous Metals Processing, 2023, 52(4): 17-25.
[11] 曹安斋. 铝合金内腔带筋筒形挤压件成形工艺分析与实验研究[D]. 太原: 中北大学, 2008.
CAO A Z.The Technology Analysis and Experimental Research on Round Extrusion Part with Intra-cavity Rib Forming of Aluminum Alloy[D]. Taiyuan: North University of China, 2008.
[12] 宋春丽, 裴小龙, 陈利文, 等. 大型薄壁复杂铝合金舱体件低压铸造模拟对比分析[J]. 特种铸造及有色合金, 2023, 43(6): 794-799.
SONG C L, PEI X L, CHEN L W, et al.Comparison Analysis of Low Pressure Casting Simulation of Large Thin-Wall Complex Aluminum Alloy Cabin[J]. Special Casting & Nonferrous Alloys, 2023, 43(6): 794-799.
[13] 申世军, 陆皓, 倪勇军, 等. 2219铝合金网格壁板增量成形有限元仿真[J]. 塑性工程学报, 2014, 21(2): 71-75.
SHEN S J, LU H, NI Y J, et al.Finite Element Simulation of Incremental Forming for 2219 Aluminium Integrally Stiffened Panel[J]. Journal of Plasticity Engineering, 2014, 21(2): 71-75.
[14] 孟佳杰, 徐晨, 徐琅, 等. 含凸台铝合金壁板垫板压弯成形规律分析[J]. 上海航天(中英文), 2024, 41(S2): 22-30.
MENG J J, XU C, XU L, et al.Analysis of Bending Forming Law of Aluminum Alloy Wall Plate with Boss[J]. Aerospace Shanghai (Chinese & English), 2024, 41(S2): 22-30.
[15] 于忠奇, 王凤琪, 戴冬华, 等. 带筋薄壁筒体类构件流动旋压技术研究进展[J]. 塑性工程学报, 2021, 28(8): 1-10.
YU Z Q, WANG F Q, DAI D H, et al.A Review of Flow Spinning Technology of Stiffened Thin-Walled Cylinders[J]. Journal of Plasticity Engineering, 2021, 28(8): 1-10.
[16] MARINI D, CUNNINGHAM D, XIROUCHAKIS P, et al.Flow Forming: A Review of Research Methodologies, Prediction Models and Their Applications[J]. International Journal of Mechanical Engineering and Technology, 2016, 7(5): 285-315.
[17] 曾祥. 铝合金纵横内筋筒形件流动旋压成形与组织演变研究[D]. 西安: 西北工业大学, 2021.
ZENG X.Study on Flow Spinning Forming and Microstructure Evolution of Aluminum Alloy Tubular Part with Longitudinal and Transverse Inner Ribs[D]. Xi’an: Northwestern Polytechnical University, 2021.
[18] ZHAN M, YANG H, GUO J, et al.Review on Hot Spinning for Difficult-to-Deform Lightweight Metals[J]. Transactions of Nonferrous Metals Society of China, 2015, 25(6): 1732-1743.
[19] 李晓凯. 带内筋筒形件超声辅助旋压实验与仿真研究[D]. 上海: 上海交通大学, 2020.
LI X K.Experiment and Simulation Study on Inner Ribbed Cylindrical Parts Spinning with Ultrasonic Vibration[D]. Shanghai: Shanghai Jiao Tong University, 2020.
[20] 周敏, 杜勇, 曾权, 等. 带横向内筋张紧轮旋压成形分析[J]. 精密成形工程, 2015, 7(2): 66-70.
ZHOU M, DU Y, ZENG Q, et al.Spinning Forming Analysis of Tension Wheel with Transverse Inner Ribs[J]. Journal of Netshape Forming Engineering, 2015, 7(2): 66-70.
[21] JIANG S Y, ZHENG Y F, REN Z Y, et al.Multi-Pass Spinning of Thin-Walled Tubular Part with Longitudinal Inner Ribs[J]. Transactions of Nonferrous Metals Society of China, 2009, 19(1): 215-221.
[22] ABD-ELTWAB A A, EL-ABDEN S Z, AHMED K I E, et al. An Investigation into Forming Internally-Spline Sleeves by Ball Spinning[J]. International Journal of Mechanical Sciences, 2017, 134: 399-410.
[23] 写旭, 韩冬, 尚勇, 等. 带环向内筋筒形件旋压成形工艺试验及缺陷分析[J]. 航天制造技术, 2022(5): 62-65.
XIE X, HAN D, SHANG Y, et al.Spinning Process Test and Defect Analysis of Cylindrical Parts with Circumferential Inner Ribs[J]. Aerospace Manufacturing Technology, 2022(5): 62-65.
[24] 朱恩锐, 崔霞, 郭陆陆, 等. TB6钛合金筒形件强力旋压成形工艺模拟[J]. 锻压技术, 2023, 48(2): 126-134.
ZHU E R, CUI X, GUO L L, et al.Simulation on Power Spinning Process for TB6 Titanium Alloy Cylindrical Parts[J]. Forging & Stamping Technology, 2023, 48(2): 126-134.
[25] LYU W, ZHAN M, GAO P F, et al.Rib Filling Behavior in Flow Forming of Thin-Walled Tube with Helical Grid-Stiffened Ribs[J]. The International Journal of Advanced Manufacturing Technology, 2022, 119(5): 2877-2894.

基金

国防基础科研计划(JCKY2022203C049)

PDF(2652 KB)

Accesses

Citation

Detail

段落导航
相关文章

/