Mechanical and Fatigue Properties of a Laser Powder Bed Fusion Ti6Al4V Alloy: A Review

Laser Powder Bed Fusion (LPBF) enables the manufacturing of complex Ti6Al4V components, but the resulting mechanical and fatigue responses are condition-dependent. This critical narrative review examines how alloy grade and interstitial chemistry, powder history, processing, microstructure, residual stress, defect population, surface condition and post-processing affect quasi-static behaviour and low-, high- and very-high-cycle fatigue behaviour. Reported properties are compared with the associated material and test data, including surface condition, build orientation, stress ratio, loading mode, stress definition and run-out criterion. The review distinguishes finite-life fatigue strength from a demonstrated fatigue limit and separates stress-life data from strain-life and crack-growth parameters. The resulting condition-specific synthesis is intended to support engineering comparison and numerical modelling without treating LPBF Ti6Al4V as a single universal material dataset.

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Publication Details

Journal
Materials
Published
2026-11-09
DOI
https://doi.org/10.3390/ma19214752
Primary Topic
Additive Manufacturing Materials and Processes
Type
article
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article

Mechanical and Fatigue Properties of a Laser Powder Bed Fusion Ti6Al4V Alloy: A Review

Srečko Glodež, Branko Nečemer, Žiga Žnidarič
Materials
Additive Manufacturing Materials and Processes
article

Mechanical and Fatigue Properties of a Laser Powder Bed Fusion Ti6Al4V Alloy: A Review

Srečko Glodež, Branko Nečemer, Žiga Žnidarič
article en

Abstract

Laser Powder Bed Fusion (LPBF) enables the manufacturing of complex Ti6Al4V components, but the resulting mechanical and fatigue responses are condition-dependent. This critical narrative review examines how alloy grade and interstitial chemistry, powder history, processing, microstructure, residual stress, defect population, surface condition and post-processing affect quasi-static behaviour and low-, high- and very-high-cycle fatigue behaviour. Reported properties are compared with the associated material and test data, including surface condition, build orientation, stress ratio, loading mode, stress definition and run-out criterion. The review distinguishes finite-life fatigue strength from a demonstrated fatigue limit and separates stress-life data from strain-life and crack-growth parameters. The resulting condition-specific synthesis is intended to support engineering comparison and numerical modelling without treating LPBF Ti6Al4V as a single universal material dataset.

MaterialsVol. 19(21)
University of Maribor (SI)
Additive Manufacturing Materials and Processes
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