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Title:Crack analysis and structural optimization on incremental press bending process for non-uniform thickness plate of 2195 aluminum-lithium alloy
Authors: Chen Lele1  Hu Deyou1  Nan Kangbin2  Han Yunqi2  Lou Shumei2  Chu Guannan3 
Unit: 1. Tianjin Aerospace Long March Vehicle Manufacturing Co.  Ltd.  Tianjin 300462 China 2.Department of Intelligent Equipment  Shandong University of Science and Technology  Tai′an 271019  China  3.School of Materials Science and Engineering  Harbin Institute of Technology (Weihai) 
KeyWords: 2195 aluminum-lithium alloy  non-uniform thickness plate  incremental press bending  crack stress concentration 
ClassificationCode:TG386
year,vol(issue):pagenumber:2025,50(7):67-73
Abstract:

 For the cracks occurred at the intersection of bosses, holes and ribs in the incremental press bending process for non-uniform thickness plate of 2195 aluminum-lithium alloy, the finite element analysis was performed by ABAQUS, and it was determined that these cracks were generated by the shear deformation caused by shear force and the stress state at the fracture location was triaxial tensile stress, which accelerated the fracture of the plate. Then, based on the simulation results and production conditions, it was proposed to alleviate the uneven stress distribution and the shear plastic deformation caused by excessive thickness differences through a gradual thickness transition in skin at the blank boss interface, which enhanced the structural strength and stability of this area and reduced the fracture risk caused by stress concentration. Furthermore, the optimized scheme was subjected to finite element analysis by ABAQUS. The results show that the distributions of Mises equivalent stress, normal stress and shear stress after optimization are more uniform. The stress at the original crack location is significantly reduced, the crack resistance of the material is effectively improved, and the products meeting the requirements are processed.

Funds:
AuthorIntro:
作者简介:陈乐乐(1986-),女,硕士,工程师 E-mail:chenlele86@126.com 通信作者:娄淑梅(1979-),女,博士,教授 E-mail:msl7119@163.com
Reference:

 [1]申世军,倪勇军,齐海雁,等.2219铝锂合金网格壁板增量成形有限元仿真[J].塑性工程学报,201421(2):71-75.


 


Shen S JNi Y JQi H Yet al. Finite element simulation of incremental forming for 2219 aluminium integrally stiffened panel[J].Journal of Plasticity Engineering201421(2):71-75.


 


[2]李卫东,万敏,阎昱.整体壁板压弯成形中性层及回弹解析[J].塑性工程学报,201421(5):156-161.


 


Li W DWan MYan Y.Neutral layer and springback analysis in press bend forming of aircraft integral panels[J].Journal of Plasticity Engineering201421(5):156-161.


 


[3]Yan YWan MWang H.FEM equivalent model for press bend forming of aircraft integral panel[J].Transactions of Nonferrous Metals Society of China200919:414-421.


 


[4]赖松柏,于登云,陈同祥.整体壁板结构弯曲成形分析的等效塑性模型[J].宇航学报,201233(6):809-815.


 


Lai S BYu D YChen T X.Plastic equivalent model for integrally stiffened panel in bending forming[J].Journal of  Astronautics201233(6):809-815.


 


[5]Yan YWang H BWan M.Prediction of stiffener buckling in press bend forming of integral panels [J].Transactions of Nonferrous Metals Society of China 201121(11):2459-2465.


 


[6]Yan YWang H BWan M.Prediction of fracture in press bend forming of aluminum alloy highstiffener integral panels [J].Computational Materials Science201150(7):2232-2244.


 


[7]张敏,田锡天,李波.整体壁板压弯成形的形状控制[J].航空学报,202041(7):66-77.


 


Zhang MTian X TLi B.Shape control for press bend forming of integral panels[J].Acta Aeronautica et Astronautica Sinica 202041(7):66-77.


 


[8]王忠堂,吴凯琦,张宏亮,.AZ31镁合金网格式壁板级进压弯成形试验研究[J].热加工工艺,202352(3):88-91.


 


Wang Z TWu K QZhang H L,et al.Experrimental study on progressive compression bending of AZ31 magnesium alloy grid panel[J].Hot Working Technology202352(3):88-91.


 


[9]刘相柱,陈沛,刘晓,.航天器X型整体壁板加工变形控制技术研究[J].机械科学与技术,202342(2):223-230.


 


Liu X ZChen PLiu Xet al.Study on deformation control technology of Xshape integral panel for spacecraft[J].Mechanical Science and Technology for Aerospace Engineering202342(2):223-230.


 


[10]乐晨,曹昱,杨帆,.基于Abaqus的等边三角形网格加筋壳建模分析方法及试验验证研究[J].导弹与航天运载技术,2019(2):12-16.


 


Le CCao YYang Fet al.The analysis method and experimental verification of isogrid stiffened shell based on Abaqus[J].Missiles and Space Vehicles2019(2):12-16.


 


[11]Muoz C Leon, Kohlgrüber D, Langrand B.Analysis of fuselage skin reinforcements with beam element models in flexible aircraft panels for ditching simulations[J].IOP Conference Series:Materials Science and Engineering20211024(1):012054.


 


[12]Boitsov V BGavva M LEndogur I A et al.Stressstrain state and buckling problems of structurallyanisotropic aircraft panels made of composite materials in view of production technology[J].Russian Aeronautics201861(4):524-532.


 


[13]章润喆,马云龙,刘丹阳,. 2195铝锂合金力学性能和组织与冷热变形过程的相关性[J].稀有金属, 2021,45(2):129-136.


 


Zhang R Z,Ma Y L,Liu D Y,et al. Dependence of mechanical properties and microstructures of 2195 AlLi alloy on cold and hot deformation process[J]. Chinese Journal of Rare Metals, 2021,45(2):129-136.


 


[14]马雪菲,王赫男,鄂顺,. 化学转化处理时间对2198铝锂合金硝酸铈转化膜耐蚀性的影响[J]. 稀有金属, 2023,47(11):1477-1485.


 


Ma X F,Wang H N,E S,et al. Corrosion resistance of Ce(NO3)3 conversion film on 2198 AlLi alloy with different chemical conversion time[J]. Chinese Journal of Rare Metals,2023,47(11):1477-1485.


 


[15]王文波,闫亮明,胡强,. 冷却预处理对7055铝合金板材组织与晶间腐蚀性能的影响[J].稀有金属, 2024,48(10):1378-1387.


 


Wang W B,Yan L M,Hu Q,et al.Microstructures and intergranular corrosion properties of 7055 alloy plate with cooling pretreatment[J]. Chinese Journal of Rare Metals, 2024,48(10):1378-1387.


 


[16]甘国强,李萍,薛克敏. 汽车件高强铝合金板件热冲压工艺研究进展[J]. 稀有金属, 2024,48(4):564-574.


 


Gan G Q,Li P,Xue K M. Research progress on hot stamping process of high strength aluminum alloy plates for automotive parts[J]. Chinese Journal of Rare Metals, 2024,48(4):564-574.


 


[17]张景新,郭沛欣,白杰.先进铝锂合金机身壁板结构承载能力研究[J].航空科学技术,2013(3):23-26.


 


Zhang J XGuo P XBai J.Strength evaluation of advanced aluminumlithium fuselage panels[J].Aeronautical Science & Technology2013(3):23-26.

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