Anisotropy of Microstructure and Tensile Properties of AlSi10Mg Formed by Selective Laser Melting

被引:10
|
作者
Hou Wei [1 ]
Chen Jing [1 ]
Chu Songlin [1 ]
Wang Xiuzhuan [1 ]
Yang Zhiyi [1 ]
Zhang Yuqi [1 ]
Teng Weibin [1 ]
机构
[1] AECC Aero Engine Control Syst Inst, Joint Lab 3D Enable Res & Dev Technol, Wuxi 214063, Jiangsu, Peoples R China
来源
关键词
materials; selective laser melting; AlSi10Mg; anisotropy; microstructure; tensile property;
D O I
10.3788/CJL201845.0702003
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Selective laser melting(SLM) technology is adopted to form AlSi10Mg alloy and the microstructure and tensile property at room temperature arc studied. The results show that SLM formed AlSi10Mg alloy has fine microstructure and high room temperature tensile properties, and the microstructure and strength show obvious anisotropy. The high cooling rate in SLM process refine the previous alpha-Al dendrites significantly, and the different solidification conditions in the core and boundary of melt pool can not only lead to different scales of a-Al dendrites, but determine the growth morphology of alpha-Al dendrites, which follows the law of epitaxial growth. Combination of the morphology and evolution of Al-Si eutectic structure of sample in different orientations, the anisotropy of microstructure is investigated. Furthermore, the strength of tensile samples along deposition (L) and scanning (T) directions is almost the same, while the elongation shows double relationship, so the different mechanical properties arc due to its anisotropy of ductility. The SEM morphology of tensile fracture presents the crack mechanism, the size of the dimple, morphology of Al-Si eutectic structure and formation of micro cracks prove that the crack mode is intergranular fracture. The experimental results show that the microstructure and properties of SLM formed AiSi10Mg arc higher than those of conventional cast components, which make SLM technology realizable in engineering application of typical components manufacturing in the field of aero engine control system.
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页数:11
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