Fatigue Crack Growth and Threshold Behavior of DMLS Ti6Al4V

Article Preview

Abstract:

Growth of long fatigue cracks in Ti6Al4V alloy manufactured by direct metal laser sintering (DMLS) was investigated. Two DMLS systems, EOSINT M270 and EOSINT M290, with different process parameters were used for production of CT specimens having three different orientations of crack propagation with respect to the DMLS build direction. The as-built specimens were stress relieved at 740 °C. The fatigue crack growth curve and the threshold values of the stress intensity factor for crack propagation were experimentally determined. It has been found that the chosen DMLS processing parameters and the used stress relieving procedure results in material exhibiting isotropic crack growth behavior, i.e. the crack growth was found to be independent of the DMLS build direction. The fatigue crack growth rates and the threshold values for the crack growth were compared with published results characterizing the as-built material and material after different post processing heat treatments.

You might also be interested in these eBooks

Info:

Periodical:

Solid State Phenomena (Volume 267)

Pages:

157-161

Citation:

Online since:

October 2017

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2017 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] B.L. Boyce, R.O. Ritchie, Effect of load ratio and maximum stress intensity on the fatigue threshold in Ti-6Al-4V, Eng. Fract. Mech. 68 (2001) 129-147.

DOI: 10.1016/s0013-7944(00)00099-0

Google Scholar

[2] Y. Okazaki, Comparison of fatigue properties and fatigue crack growth rates of various implantable metals, Materials 5 (2012) 2981-3005.

DOI: 10.3390/ma5122981

Google Scholar

[3] H. Oguma, T. Nakamura, Fatigue crack propagation properties of Ti–6Al–4V in vacuum environments, Int. J. Fatigue 50 (2013) 89-93.

DOI: 10.1016/j.ijfatigue.2012.02.012

Google Scholar

[4] T.H. Becker, M. Beck, C. Scheffer, Microstructure and mechanical properties of direct metal laser sintered Ti-6Al-4V, S. Afr. J. Ind. Eng. 26 (2015) 1-10.

DOI: 10.7166/26-1-1022

Google Scholar

[5] R. Konečná, L. Kunz, A. Bača, G. Nicoletto, Long fatigue crack growth in Ti6Al4V produced by direct metal laser Sintering, Procedia Engineer. 160 (2016) 69-76.

DOI: 10.1016/j.proeng.2016.08.864

Google Scholar

[6] V. Cain, L. Thijs, J. Van Humbeeck, B. Van Hooreweder, R. Knutsen, Crack propagation and fracture toughness of Ti6Al4V alloy produced by selective laser melting, Add. Man. 5 (2015) 68-76.

DOI: 10.1016/j.addma.2014.12.006

Google Scholar

[7] C.R. Knowles, T.H. Becker, R.B. Tait, Residual stress measurements and structural integrity implications for selective laser melted Ti-6Al-4V, S. Afr. J. Ind. Eng. 23 (2012) 119-129.

DOI: 10.7166/23-3-515

Google Scholar

[8] M. Klesnil, P. Lukáš, Fatigue of Metallic Materials, Elsevier, Amsterdam (1992).

Google Scholar

[9] S. Leuders, M. Thöne, A. Riemer, T. Niendorf, T. Tröster, H.A. Richard, H.J. Maier, On the mechanical behaviour of titanium alloy TiAl6V4 manufactured by selective laser melting: Fatigue resistance and crack growth performance, Int. J. Fatigue 48 (2013).

DOI: 10.1016/j.ijfatigue.2012.11.011

Google Scholar