Simulation of fatigue small crack growth in additive manufactured Ti-6Al-4V material

被引:18
作者
Gupta, A. [1 ,2 ]
Sun, W. [2 ]
Bennett, C. J. [2 ]
机构
[1] Rolls Royce Plc, Derby DE24 8BJ, England
[2] Univ Nottingham, Fac Engn, G2TRC, Univ Pk, Nottingham NG7 2RD, England
基金
英国工程与自然科学研究理事会;
关键词
Selective laser melting; Fatigue; Physically small cracks; Crack growth; Defects; Ti-6Al-4V; NEAR-THRESHOLD FATIGUE; LIFE PREDICTION; BEHAVIOR; TITANIUM; PROPAGATION; DESIGN; RESISTANCE; METALS; ISSUES; MODEL;
D O I
10.1007/s00161-020-00878-0
中图分类号
O414.1 [热力学];
学科分类号
摘要
Additive manufacturing (AM) offers design freedom and ability to fabricate parts of complex shapes which are not often possible with the conventional methods of manufacturing. In an AM part, even with optimum build parameters, a complete elimination of defects is not possible and this makes it hard to fully deploy the AM technology to build load bearing parts operating under cyclic loading conditions. Many of these defects are < 1 mm in size and are categorised as 'small cracks'. Local interaction of cracks with microstructural features and closure effects at the wake of the crack tip are some of the factors which make the growth behaviour of small and long cracks different. A crack growth life prediction method, which effectively considers the small crack growth behaviour, has been discussed in this paper. This proposed method includes a detailed finite element-based crack growth simulation using the ANSYS SMART fracture technology. The lifing calculations utilise the modified NASGRO equation and small crack growth data which was obtained from the published long crack growth data, corrected for closure effects. The predicted stress versus number of cycles curves were compared against the fatigue test results for the AM specimens in Ti-6Al-4V material. A good correlation between the predictions and test results suggests that the proposed method can be used to assess the small crack growth life of AM parts where the fatigue effects of cyclic loading can be quite significant.
引用
收藏
页码:1745 / 1761
页数:17
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