Numerical simulation of the fatigue behavior of additive manufactured titanium porous lattice structures

被引:103
|
作者
Zargarian, A. [1 ]
Esfahanian, M. [1 ]
Kadkhodapour, J. [2 ,3 ]
Ziaei-Rad, S. [1 ]
机构
[1] Isfahan Univ Technol, Dept Mech Engn, Esfahan 8415683111, Iran
[2] Shahid Rajaee Teacher Training Univ, Dept Mech Engn, Tehran, Iran
[3] Univ Stuttgart, Inst Mat Testing Mat Sci & Strength Mat IMWF, D-70174 Stuttgart, Germany
关键词
Finite element; Fatigue; Additive manufacturing; Cellular solids; Ti6Al4V ELI; COMPRESSION-COMPRESSION FATIGUE; CELL ALUMINUM FOAMS; MECHANICAL-PROPERTIES; CRACK PROPAGATION; MELTED TI-6AL-4V; BIOMATERIALS; METALS; ALLOY; PERFORMANCE; FABRICATION;
D O I
10.1016/j.msec.2015.11.054
中图分类号
TB3 [工程材料学]; R318.08 [生物材料学];
学科分类号
0805 ; 080501 ; 080502 ;
摘要
In this paper, the effects of cell geometry and relative density on the high-cycle fatigue behavior of Titanium scaffolds produced by selective laser melting and electron beam melting techniques were numerically investigated by finite element analysis. The regular titanium lattice samples with three different unit cell geometries, namely, diamond, rhombic dodecahedron and truncated cuboctahedron, and the relative density range of 0.1-03 were analyzed under uniaxial cyclic compressive loading. A failure event based algorithm was employed to simulate fatigue failure in the cellular material. Stress-life approach was used to model fatigue failure of both bulk (struts) and cellular material. The predicted fatigue life and the damage pattern of all three structures were found to be in good agreement with the experimental fatigue investigations published in the literature. The results also showed that the relationship between fatigue strength and cycles to failure obeyed the power law. The coefficient of power function was shown to depend on relative density, geometry and fatigue properties of the bulk material while the exponent was only dependent on the fatigue behavior of the bulk material. The results also indicated the failure surface at an angle of 45 to the loading direction. (C) 2015 Elsevier B.V. All rights reserved.
引用
收藏
页码:339 / 347
页数:9
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