The influence of porosity on Ti-6Al-4V parts fabricated by laser powder bed fusion in the pursuit of process efficiency

被引:18
|
作者
Kan, Wen Hao [1 ,2 ]
Gao, Mu [1 ,2 ]
Zhang, Xi [3 ]
Liang, Enquan [3 ]
Chiu, Ngai Sum Louis [1 ,2 ]
Lim, Chao Voon Samuel [1 ,2 ]
Huang, Aijun [1 ,2 ]
机构
[1] Monash Ctr Addit Mfg, Notting Hill, Vic 3168, Australia
[2] Monash Univ, Dept Mat Sci & Engn, Clayton, Vic 3800, Australia
[3] Commercial Aircraft Corp China Ltd, Shanghai 200050, Peoples R China
关键词
Additive manufacturing; Titanium alloys; Mechanical properties; Porosity; Process efficiency; MECHANICAL-PROPERTIES; TENSILE PROPERTIES; MARTENSITE DECOMPOSITION; SURFACE-ROUGHNESS; IMPACT PROPERTIES; RESIDUAL-STRESS; FATIGUE; STRENGTH; BEHAVIOR; DENSITY;
D O I
10.1007/s00170-021-08374-8
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this study, the influence that porosities play on the mechanical properties of Ti-6Al-4V parts fabricated by laser powder bed fusion (LPBF) was investigated with the aim of improving process efficiency of the LPBF process by establishing the resulting trade-offs to component quality. It was found that build times can be substantially reduced by using higher layer thickness parameters without a significant detriment to mechanical properties. Where porosities formed, spherical pores tend to have a marginal effect on Young's modulus, yield strength, tensile strength, and uniform elongation as these properties can be approximated linearly using the rule of mixtures assuming null strength pores. However, such pores were found to be otherwise more detrimental to total elongation and toughness. Conversely, lack of fusion pores are extremely detrimental and should be avoided. Thus, it is proposed that when building a component, different process parameters can be used at different regions of the component to maximize process efficiency without compromising its overall function. For instance, for surfaces, a highly optimized parameter set with lower layer thickness can be used. At regions with minimal stress distribution during service, a large layer thickness parameter set where the resulting mechanical properties is sufficient can be used.
引用
收藏
页码:5417 / 5438
页数:22
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