Journal of Jilin University(Engineering and Technology Edition) ›› 2021, Vol. 51 ›› Issue (3): 847-854.doi: 10.13229/j.cnki.jdxbgxb20200180

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Effect of hot forming on static mechanical properties of AA5754 aluminum alloy

Wei-min ZHUANG1(),Peng-yue WANG1,Rui-juan GAO2,Dong-xuan XIE3   

  1. 1.State Key Laboratory of Automotive Simulation and Control,Jilin University,Changchun 130022,China
    2.Department of Mechanical and Electrical Engineering,Taiyuan University,Taiyuan 030032,China
    3.FAW-Volkswagen Automotive Co. ,Ltd. ,Changchun 130011,China
  • Received:2020-02-18 Online:2021-05-01 Published:2021-05-07

Abstract:

The effects of thermal deformation on the failure strain, ultimate stress, and yield stress of AA5754 aluminum alloy are analyzed by high temperature pre-tension test and room temperature tensile test. A damage coupling pre-forming constitutive model is established to characterize the relationship between forming strain and service performance. This constitutive model is used to analyze the effects of forming damage and thickness change on the bending performance of side-door impact beam. The results show that forming damage directly reduces the service performance of AA5754 aluminum alloy. When the forming strain is 0.7 at 300 ℃, the failure strain and ultimate stress are reduced by 62% and 16%, respectively. The proposed constitutive model can accurately predict the effect of hot forming on the static mechanical properties of AA5754 aluminum alloy.

Key words: vehicle engineering, AA5754 aluminum alloy, side-door impact beam, hot forming, constitutive model

CLC Number: 

  • U463.82

Fig.1

Geometry of specimen"

Fig.2

MMS-200 thermal simulation machine"

Table 1

Scheme of thermal pre-tension test"

温度

/°C

参数应变比率失效
00.30.50.7
300应变量/mm00.1530.2540.3560.509
拉伸量/mm01.8333.2204.7557.372
400应变量/mm00.1810.3030.4240.606
拉伸量/mm02.2163.9345.8739.260

Fig.3

Thermal pre-tensile test procedure"

Fig.4

Results of thermal pre-tensile test"

Fig.5

Results of tensile test at room temperature"

Table 2

Cross-sectional area of specimen afterthermal pre-tension test"

应变比率温度/℃
300400
0.029.8229.80
0.327.0424.82
0.524.7821.37
0.721.8317.78

Fig.6

Stress-strain curve of tensile testat room temperature"

Fig.7

Relationship between forming strain and failure strain, ultimate stress and yield stress"

Table 3

Constants of damage-coupling pre-forming constitutive model"

材料常数数值材料常数数值
K071.904η17.9862
k043.53Δ00.25
n1.8Δ10.013
B389.3Δ21.3135
ξ02.3095E7.055×104
ξ10.9238

Fig.8

Comparison of stress-strain curves betweenexperiment (solid curve) andcomputation(symbol)"

Fig.9

Comparison of simulation and experiment of thermal tensile with forming strain 0.5"

Fig.10

Comparison of simulation and DICtest result with forming strain 0.5"

Fig.11

Comparison of force-displacement curves with different forming strain between experimental(solid curve) and numerical(symbol) results"

Fig.12

Section size of side-door impact beam"

Fig.13

Distribution thickness and damage in cross-section of side-door impact beam"

Fig.14

Three-point bending simulation model"

Fig.15

Effect of thickness and damage on load- displacement and load reduction ratio"

Table 4

Ultimate bending load and failure displacement of side-door impact beam"

模型A模型B模型C
最大载荷/N298428302713
失效位移/mm164150138

Fig.16

Effect of thickness and damage on energy-displacement and energy reduction ratio"

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