采用0.2 mm Al+5 mm Mg+0.2 mm Al的组坯方式,400℃保温10 min热轧制得大厚度比Al/Mg/Al层合板,研究了压下率对其界面结合、镁基材组织及拉伸性能的影响。对压下率为41%、49%和60%热轧制备的Al/Mg/Al层合板进行了界面SEM观察、微观组织...采用0.2 mm Al+5 mm Mg+0.2 mm Al的组坯方式,400℃保温10 min热轧制得大厚度比Al/Mg/Al层合板,研究了压下率对其界面结合、镁基材组织及拉伸性能的影响。对压下率为41%、49%和60%热轧制备的Al/Mg/Al层合板进行了界面SEM观察、微观组织观察、拉伸实验及拉伸断口的观察。结果表明,大厚度比Al/Mg/Al层合板在压下率为60%时,边部的附加拉应力造成边裂的出现;经41%压下率热轧可实现界面结合,但存在微缺陷,压下率为49%及以上可实现良好结合;压下率对Al/Mg/Al层合板的屈服强度和抗拉强度影响较小,对其伸长率影响较大。随着压下率增加,伸长率先增加后减小。压下率为49%时,伸长率最大为26%,其原因在于该工艺下镁基材的晶粒均匀细小,韧性提高。展开更多
In-situ bending and stretching were conducted on hot-rolled and annealed Ti/Al/Mg/Al/Ti laminates,with a focus on crack initiation and propagation of intermetallics and component layers,which helps to clarify their de...In-situ bending and stretching were conducted on hot-rolled and annealed Ti/Al/Mg/Al/Ti laminates,with a focus on crack initiation and propagation of intermetallics and component layers,which helps to clarify their deformation behavior and fracture forms.The results show that delamination is the early fracture form of laminate with or without intermetallics at Al/Mg interface,so Al/Mg interfacial bonding strength determines the mechanical properties of laminate.Various and irregular intermetallics cracks lead to Al/Mg interface delamination in annealed laminate and help to release stress.Necking and fracture of component layers are observed at the late deformation stage,and the sequence is Al,Mg and Ti layers,resulting from their strength.Angle between crack propagation direction and stretching direction of Mg layer both in rolled and annealed laminates is around 45°due to the effect of shear deformation,and crack convergence leads to final complete fracture of Mg layer.展开更多
基金supported by the National Key Research and Development Program of China(No.2018YFA0707300)the General Program of National Natural Science Foundation of China(No.51905372)+1 种基金the Key Project of Shanxi Province,China(No.20181101008)the Postdoctoral Science Foundation of China(No.2020T130463)。
文摘采用0.2 mm Al+5 mm Mg+0.2 mm Al的组坯方式,400℃保温10 min热轧制得大厚度比Al/Mg/Al层合板,研究了压下率对其界面结合、镁基材组织及拉伸性能的影响。对压下率为41%、49%和60%热轧制备的Al/Mg/Al层合板进行了界面SEM观察、微观组织观察、拉伸实验及拉伸断口的观察。结果表明,大厚度比Al/Mg/Al层合板在压下率为60%时,边部的附加拉应力造成边裂的出现;经41%压下率热轧可实现界面结合,但存在微缺陷,压下率为49%及以上可实现良好结合;压下率对Al/Mg/Al层合板的屈服强度和抗拉强度影响较小,对其伸长率影响较大。随着压下率增加,伸长率先增加后减小。压下率为49%时,伸长率最大为26%,其原因在于该工艺下镁基材的晶粒均匀细小,韧性提高。
基金supported by the National Natural Science Foundation of China (No. 51505323)the Applied Basic Research Program of Shanxi Province,China (Nos. 20210302123117, 20210302124658)。
基金financially supported by Shanxi provincial Youth Fund(No.201801D221101)the National Natural Science Foundation of China(Nos.52005362,U1810208,U1710254)Scientific and Technological Innovation Programs of Higher Education Institutions in Shanxi,China(Nos.2019L0149,2019L0994)。
文摘In-situ bending and stretching were conducted on hot-rolled and annealed Ti/Al/Mg/Al/Ti laminates,with a focus on crack initiation and propagation of intermetallics and component layers,which helps to clarify their deformation behavior and fracture forms.The results show that delamination is the early fracture form of laminate with or without intermetallics at Al/Mg interface,so Al/Mg interfacial bonding strength determines the mechanical properties of laminate.Various and irregular intermetallics cracks lead to Al/Mg interface delamination in annealed laminate and help to release stress.Necking and fracture of component layers are observed at the late deformation stage,and the sequence is Al,Mg and Ti layers,resulting from their strength.Angle between crack propagation direction and stretching direction of Mg layer both in rolled and annealed laminates is around 45°due to the effect of shear deformation,and crack convergence leads to final complete fracture of Mg layer.
