An investigation of creep age forming of AA7B04 stiffened plates: Experiment and FE modelling

被引:32
作者
Lyu, Fenggong [1 ,2 ,3 ,4 ]
Li, Yong [2 ]
Huang, Xia [1 ,3 ,4 ]
Shi, Zhusheng [2 ]
Zeng, Yuansong [1 ,3 ,4 ]
Lin, Jianguo [2 ]
机构
[1] AVIC Mfg Technol Inst, Beijing 100024, Peoples R China
[2] Imperial Coll London, Dept Mech Engn, London SW7 2AZ, England
[3] Aeronaut Key Lab Plast Forming Technol, Beijing 100024, Peoples R China
[4] Beijing Key Lab Digital Plast Forming & Equipment, Beijing 100024, Peoples R China
基金
英国工程与自然科学研究理事会;
关键词
Creep age forming; Precipitate; Aluminium alloy 7B04; Constitutive modelling; Stiffened plate; Numerical simulation; AGING BEHAVIOR; SPRINGBACK; ALLOY; STRESS; AA2050; PANEL;
D O I
10.1016/j.jmapro.2018.11.031
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Creep age forming (CAF) of aluminium alloy 7B04 (AA7B04) stiffened plates has been experimentally and numerically investigated in this study. Creep-ageing experiments of AA7B04-T651 were conducted under different tensile stress levels at 140 degrees C for up to 20 h, and a set of unified constitutive equations was calibrated based on the experimental results of the evolutions of creep strain, yield strength and precipitate size, which was implemented into ABAQUS for CAF process modelling. CAF experiments and corresponding simulations of AA7B04 stiffened plates were then carried out and the effect of stiffener height and die radius on springback and yield strength was studied. It was found that the springback percentage decreases with increasing stiffener height and decreasing forming die radius, and the yield strength is slightly lower in the stiffener than in the skin of the CAFed stiffened plates due to stress effect on ageing progression. A good agreement has been achieved between experimental and corresponding FE results, with maximum deviations of 6.7% and 3.3% respectively for springback and yield strength.
引用
收藏
页码:232 / 241
页数:10
相关论文
共 29 条
[1]  
Brewer H, 1989, AIRCR DES OP M, P2087
[2]   Stress relaxation behavior of an Al-Zn-Mg-Cu alloy in simulated age-forming process [J].
Chen, J. F. ;
Jiang, J. T. ;
Zhen, L. ;
Shao, W. Z. .
JOURNAL OF MATERIALS PROCESSING TECHNOLOGY, 2014, 214 (04) :775-783
[3]   Recent developments in advanced aircraft aluminium alloys [J].
Dursun, Tolga ;
Soutis, Costas .
MATERIALS & DESIGN, 2014, 56 :862-871
[4]   Numerical modeling of integrally stiffened structures forming from creep age forming technique [J].
Guines, D. ;
Gavrus, A. ;
Ragneau, E. .
INTERNATIONAL JOURNAL OF MATERIAL FORMING, 2008, 1 (Suppl 1) :1071-1074
[5]   Electromagnetic incremental forming of integral panel under different discharge conditions [J].
Guo, Kun ;
Lei, Xinpeng ;
Zhan, Mei ;
Tan, Jingqiang .
JOURNAL OF MANUFACTURING PROCESSES, 2017, 28 :373-382
[6]   Constitutive modelling of primary creep for age forming an aluminium alloy [J].
Ho, KC ;
Lin, J ;
Dean, TA .
JOURNAL OF MATERIALS PROCESSING TECHNOLOGY, 2004, 153 :122-127
[7]   AUTOCLAVE AGE FORMING LARGE ALUMINUM AIRCRAFT PANELS [J].
HOLMAN, MC .
JOURNAL OF MECHANICAL WORKING TECHNOLOGY, 1989, 20 :477-488
[8]  
Inforzato DJ, 2012, MATER RES-IBERO-AM J, V15, P596, DOI [10.1590/S1516-14392012005000080, 10.1590/S1516-14392012000400018]
[9]   Material modelling and its application to creep-age forming of aluminium alloy 7B04 [J].
Lam, Aaron C. L. ;
Shi, Zhusheng ;
Huang, Xia ;
Yang, Yo-Lun ;
Zeng, Yuansong ;
Lin, Jianguo .
MANUFACTURING REVIEW, 2015, 2
[10]   Influences of residual stresses and initial distortion on springback prediction of 7B04-T651 aluminium plates in creep-age forming [J].
Lam, Aaron C. L. ;
Shi, Zhusheng ;
Lin, Jianguo ;
Huang, Xia .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2015, 103 :115-126