Measuring and Analyzing Defects of Additive Manufactured Ti‐6Al‐4V Specimens Through Image Segmentation

ABSTRACT Additive manufacturing (AM) has expanded significantly, particularly in aerospace; however, AM materials often have defects that impair fatigue performance. This study examines the geometry and morphology of critical defects in Ti‐6Al‐4V specimens produced using three printing quality settings, followed by hot isostatic pressing (HIP) or heat treatment (HT). We present an automated fatigue failure analysis framework using computer vision and AI to identify critical defects, measure surface proximity, and quantify 14 geometric and morphological features. The model achieved a mean IoU of 0.836 and approximately 10% error in feature measurement. Results show that surface proximity is the most influential factor on fatigue life, with near‐surface defects degrading performance for HT specimens with lack‐of‐fusion (LOF) defects. For HIP specimens, failure sources were typically within 0.16–0.6 mm from the surface. Additionally, for LOF defects, the ‐parameter model achieved with measured cycles to failure.

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Publication Details

Journal
Fatigue & Fracture of Engineering Materials & Structures
Published
2025-09-18
DOI
https://doi.org/10.1111/ffe.70084
Primary Topic
Additive Manufacturing Materials and Processes
Type
article
Field-Weighted Citation Impact
0.00

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Measuring and Analyzing Defects of Additive Manufactured Ti‐6Al‐4V Specimens Through Image Segmentation

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Measuring and Analyzing Defects of Additive Manufactured Ti‐6Al‐4V Specimens Through Image Segmentation

Oz Golan, Carmel Matias, Chen Hajaj, Alex Diskin, Mor Mega, Or Haim Anidjar, Ro’i Lang, Sahar Slonimsky, Strokin Evgeny
article en

Abstract

ABSTRACT Additive manufacturing (AM) has expanded significantly, particularly in aerospace; however, AM materials often have defects that impair fatigue performance. This study examines the geometry and morphology of critical defects in Ti‐6Al‐4V specimens produced using three printing quality settings, followed by hot isostatic pressing (HIP) or heat treatment (HT). We present an automated fatigue failure analysis framework using computer vision and AI to identify critical defects, measure surface proximity, and quantify 14 geometric and morphological features. The model achieved a mean IoU of 0.836 and approximately 10% error in feature measurement. Results show that surface proximity is the most influential factor on fatigue life, with near‐surface defects degrading performance for HT specimens with lack‐of‐fusion (LOF) defects. For HIP specimens, failure sources were typically within 0.16–0.6 mm from the surface. Additionally, for LOF defects, the ‐parameter model achieved with measured cycles to failure.

Fatigue & Fracture of Engineering Materials & StructuresVol. 48(12)
Afeka College of Engineering (IL), Technion – Israel Institute of Technology (IL), College of Management Academic Studies (IL), Israel Aerospace Industries (Israel) (IL), Ariel University (IL)
Israel Aerospace Industries, Ariel University
Openalex Percentile: Top 74%
Additive Manufacturing Materials and Processes
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