摘要
研究激光选区熔化(selective laser melting,SLM)技术成形Al-Mg-Sc-Zr合金材料不同取向的显微组织特征、拉伸和损伤容限性能。结果表明:YZ截面为细小的等轴晶和粗大的柱状晶组成的双峰组织,XY截面由细小的等轴晶组成;0°和90°方向屈服强度、抗拉强度均超过500 MPa,各向异性较小,但堆积层间存在的未熔合缺陷使得90°方向断裂伸长率明显低于0°方向;0°和90°CT试样K_(IC)分别为21.41 MPa·m^(1/2)和20.89 MPa·m^(1/2),在柱状晶区域裂纹扩展阻抗低,导致90°CT试样K_(IC)稍小;显微组织和缺陷是影响裂纹扩展性能各向异性的主要因素,在近门槛区未熔合缺陷起主导作用,当裂纹面平行于水平方向时裂纹扩展速率更快;在稳态扩展区显微组织的影响起主导作用,当裂纹面平行于水平方向时为穿晶断裂,裂纹扩展阻抗较高,裂纹扩展速率较低。
The microstructure,tensile and damage tolerance properties in different directions of Al-Mg-Sc-Zr alloy fabricated through selective laser melting(SLM)have been investigated.The results show that the YZ plane is a bimodal grain morphology composed of fine equiaxed grains and coarse columnar grains,while the XY plane is composed of fine equiaxed grains.The yield strength and tensile strength in both 0°and 90°directions are over 500 MPa,and the anisotropy is small,while the elongation in 90°direction is significantly lower than the 0°direction due to the lack of fusion(LOF)defects between the deposited layers.The K_(IC) of the 0°and 90°CT samples are respectively 21.41 MPa·m^(1/2) and 20.89 MPa·m^(1/2).The resistance to crack propagation in columnar grains region is lower and leading to a smaller K_(IC) for 90°CT samples.The microstructure and defects are the two main factors that affect the anisotropy of crack propagation performance.The LOF defects play a leading role in the near-threshold regime,and the crack propagation rate is faster when the crack propagation plane is parallel to transverse direction.On the other hand,the microstructure plays a leading role in the steady-state propagation regime.The fracture surface exhibits transgranular fracture when the crack propagation plane is parallel to transverse direction,which provides higher crack propagation resistance and result in lower crack propagation rate.
作者
冯振宇
陈翥仪
张雪峰
夏晓宇
邹君
FENG Zhenyu;CHEN Zhuyi;ZHANG Xuefeng;XIA Xiaoyu;ZOU Jun(Science and Technology Innovation Institute,Civil Aviation University of China,Tianjin 300300,China;Sino-European Institute of Aviation Engineering,Civil Aviation University of China,Tianjin 300300,China;AVIC Manufacturing Technology Institute,Beijing 100024,China;College of Safety Science and Engineering,Civil Aviation University of China,Tianjin 300300,China)
出处
《航空材料学报》
CAS
CSCD
北大核心
2024年第1期143-151,共9页
Journal of Aeronautical Materials
基金
机械结构力学及控制国家重点实验室开放课题(MCMS-E-0522Y03)
中央高校基金(3122022099)。