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复杂曲率铝合金薄壁构件气胀成形技术研究

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为满足复杂曲率轻量化薄壁构件快速高质量成形的需求,对5754铝合金复杂构件的气胀成形性能进行了试验与仿真研究.通过单一变量法确定了型腔气压和压边力的最佳工艺参数.结合数值模拟和成形试验,分析研究了型腔气压和压边力对构件成形性能的影响规律及成形机理.结果表明,最佳的成形气压和压边力分别为1.2 MPa和4.6 MPa.当气压小于1 MPa时,最大成形深度不断增加,最大应力位于主特征中心,壁厚分布由中心向两侧递增;当气压超过1 MPa后,最大成形深度保持不变,最大应力位于型腔中心两侧,壁厚分布由中心向两侧先减后增.当压边力小于4.3 MPa时会导致构件边缘起皱;增大压边力可有效抑制起皱,但压边力超过4.9 MPa时会增加构件局部破裂的风险.因此,采用上述最佳工艺参数能够成形质量良好的复杂曲率铝合金薄壁构件.
Study on gas forming technology for complex curvature aluminum alloy thin-walled components
With the progress and development of science and technology,the demand for industrial alloy integral thin-wall components with light weight,high strength,large size and complex shape is increasing,and the manufacturing process also has higher requirements.Because of its good plasticity and relatively low price,aluminum alloy has become an ideal material for the manufacture of parts for carrying equipment.To meet the demands of rapid and high-quality forming for lightweight thin-wall components with complex curvature,5754 thin-walled aluminum alloy members with large depth-to-diameter ratio and complex curvature characteristics are taken as the research object in this study,which employs advanced gas forming technology to experimentally and numerically investigate the forming performance of 5754 aluminum alloy complex components.Firstly,a self-designed rapid gas forming platform for sheet metal is established to conduct gas forming experiments on thin-walled components made of 5754 aluminum alloy with complex curvature.The optimal values for cavity air pressure and blank edge holding force are determined through single-variable method.Secondly,a finite element model for the gas forming of aluminum alloy thin-walled components is established using LS-DYNA software.The forming process and quality of complex-curvature thin-walled aluminum alloy components under various process parameters are examined.Finally,combining numerical simulation with experimental result data,the forming depth,wall thickness distribution,and maximum stress and strain of the sample are used as forming performance characterization parameters,and a parameter analysis is conducted to study the effects and mechanisms of cavity air pressure and blank holding force on forming performance.The results show that,in the case studied,the minimum cavity pressure required for mold sticking is 1 MPa.When the cavity air pressure is less than 1 MPa,the maximum forming depth continuously increases.The maximum stress and strain are located at the center of the main feature,and the wall thickness distribution increases from the center of the aluminum sheet towards both sides along the major axis.However,when the air pressure exceeds 1 MPa,the maximum forming depth remains constant.The maximum stress and strain are located on both sides of the center of the cavity,and the wall thickness distribution decreases first and then increases from the center of the plate to both sides along the long axis.Regarding edge holding force,when the blank holding force is less than 4.3 MPa,wrinkling defects occur on both sides of the flange and cavity.Increasing edge holding force effectively suppresses wrinkles,but it will increase the risk of local component rupture when it exceeds 4.9 MPa.Ultimately,through careful selection,the optimal forming air pressure and edge holding force are determined to be 1.2 MPa and 4.6 MPa,respectively.When the cavity pressure is 1.2 MPa,the component is fully formed and the forming quality is the best.Meanwhile,the holding force of 4.6 MPa effectively avoids defect formations such as wrinkling and cracking of the sheet. Therefore,the complex curvature aluminum alloy thin-wall components with good quality is formed by using the above optimum process parameters.

5754 aluminum alloythin-walled componentsgas formingprocess parameternumerical simulation

赵忠浩、赵喜东、亓昌、盈亮、同勃阳、杨姝、魏文涛

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大连理工大学 机械工程学院,辽宁 大连 116024

大连理工大学宁波研究院,浙江 宁波 315016

中国长峰机电技术研究设计院,北京 100854

5754 铝合金 薄壁构件 气胀成形 工艺参数 数值模拟

国家重点研发计划课题

2022YFB2503503

2024

重庆理工大学学报
重庆理工大学

重庆理工大学学报

CSTPCD北大核心
影响因子:0.567
ISSN:1674-8425
年,卷(期):2024.38(11)
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