Study of Additive Manufacturing Intrinsic Defects on Fatigue Life of Ti-6Al-4V

The present work presents a new approach to studying the structural integrity of a Ti-6Al-4V alloy obtained by Selective Laser Melting (SLM). This approach is based on the intrinsic addictive manufacturing defects analysis obtained by nanotomography, the experimental S-N curve, and the small crack growth Murakami and Endo model. Also, two counting methods of 3D manufacturing intrinsic defects were considered. The simulation of S-N curves and the small crack propagation curves were successfully obtained. New models for predicted fatigue limit were developed, one using the (3D) variable area of the defects observed as the total area and the other using the total project area. The 3D total surface area counting method presents more conservative values on crack propagation studies, so it is recommended for integrity studies of Ti6Al4V alloy obtained by SLM.

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Published
2025-05-06
DOI
https://doi.org/10.3390/engproc2025090107
Citations
1
Primary Topic
Additive Manufacturing Materials and Processes
Type
article
Field-Weighted Citation Impact
0.71

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article

Study of Additive Manufacturing Intrinsic Defects on Fatigue Life of Ti-6Al-4V

A.M. Pereira, Rui F. Martins, M.F.C. Pereira, João Bosco da Mota Alves et al.
1 citations
Additive Manufacturing Materials and Processes
0.71
article

Study of Additive Manufacturing Intrinsic Defects on Fatigue Life of Ti-6Al-4V

A.M. Pereira, Rui F. Martins, M.F.C. Pereira, João Bosco da Mota Alves, Teresa Morgado
article en
1 citations

Abstract

The present work presents a new approach to studying the structural integrity of a Ti-6Al-4V alloy obtained by Selective Laser Melting (SLM). This approach is based on the intrinsic addictive manufacturing defects analysis obtained by nanotomography, the experimental S-N curve, and the small crack growth Murakami and Endo model. Also, two counting methods of 3D manufacturing intrinsic defects were considered. The simulation of S-N curves and the small crack propagation curves were successfully obtained. New models for predicted fatigue limit were developed, one using the (3D) variable area of the defects observed as the total area and the other using the total project area. The 3D total surface area counting method presents more conservative values on crack propagation studies, so it is recommended for integrity studies of Ti6Al4V alloy obtained by SLM.

University of Lisbon (PT), Instituto Politécnico de Leiria (PT), Universidade Politécnica de Lisboa (PT), Universidade Nova de Lisboa (PT), Escola Naval (PT)
Centro de Recursos Naturais e Ambiente, Universidade de Lisboa, Universidade Nova de Lisboa, UNIDEMI, Instituto Superior Técnico
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Openalex Percentile: Top 33%
Additive Manufacturing Materials and Processes
0.71
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Study of Additive Manufacturing Intrinsic Defects on Fatigue Life of Ti-6Al-4V — A.M. Pereira, Rui F. Martins, et al. · (2025) | TGRS Research Map | TGRS