The Influence of Porosity on Fatigue Crack Initiation in Additively Manufactured Titanium Components

Abstract Without post-manufacture HIPing the fatigue life of electron beam melting (EBM) additively manufactured parts is currently dominated by the presence of porosity, exhibiting large amounts of scatter. Here we have shown that the size and location of these defects is crucial in determining the...

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Main Authors: S. Tammas-Williams, P. J. Withers, I. Todd, P. B. Prangnell
Format: Article
Language:English
Published: Nature Publishing Group 2017-08-01
Series:Scientific Reports
Online Access:https://doi.org/10.1038/s41598-017-06504-5
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spelling doaj-a34671fedf574a5b9334a973732871e52020-12-08T00:20:30ZengNature Publishing GroupScientific Reports2045-23222017-08-017111310.1038/s41598-017-06504-5The Influence of Porosity on Fatigue Crack Initiation in Additively Manufactured Titanium ComponentsS. Tammas-Williams0P. J. Withers1I. Todd2P. B. Prangnell3Department of Materials Science and Engineering, University of SheffieldSchool of Materials, University of ManchesterDepartment of Materials Science and Engineering, University of SheffieldSchool of Materials, University of ManchesterAbstract Without post-manufacture HIPing the fatigue life of electron beam melting (EBM) additively manufactured parts is currently dominated by the presence of porosity, exhibiting large amounts of scatter. Here we have shown that the size and location of these defects is crucial in determining the fatigue life of EBM Ti-6Al-4V samples. X-ray computed tomography has been used to characterise all the pores in fatigue samples prior to testing and to follow the initiation and growth of fatigue cracks. This shows that the initiation stage comprises a large fraction of life (>70%). In these samples the initiating defect was often some way from being the largest (merely within the top 35% of large defects). Using various ranking strategies including a range of parameters, we found that when the proximity to the surface and the pore aspect ratio were included the actual initiating defect was within the top 3% of defects ranked most harmful. This lays the basis for considering how the deposition parameters can be optimised to ensure that the distribution of pores is tailored to the distribution of applied stresses in additively manufactured parts to maximise the fatigue life for a given loading cycle.https://doi.org/10.1038/s41598-017-06504-5
collection DOAJ
language English
format Article
sources DOAJ
author S. Tammas-Williams
P. J. Withers
I. Todd
P. B. Prangnell
spellingShingle S. Tammas-Williams
P. J. Withers
I. Todd
P. B. Prangnell
The Influence of Porosity on Fatigue Crack Initiation in Additively Manufactured Titanium Components
Scientific Reports
author_facet S. Tammas-Williams
P. J. Withers
I. Todd
P. B. Prangnell
author_sort S. Tammas-Williams
title The Influence of Porosity on Fatigue Crack Initiation in Additively Manufactured Titanium Components
title_short The Influence of Porosity on Fatigue Crack Initiation in Additively Manufactured Titanium Components
title_full The Influence of Porosity on Fatigue Crack Initiation in Additively Manufactured Titanium Components
title_fullStr The Influence of Porosity on Fatigue Crack Initiation in Additively Manufactured Titanium Components
title_full_unstemmed The Influence of Porosity on Fatigue Crack Initiation in Additively Manufactured Titanium Components
title_sort influence of porosity on fatigue crack initiation in additively manufactured titanium components
publisher Nature Publishing Group
series Scientific Reports
issn 2045-2322
publishDate 2017-08-01
description Abstract Without post-manufacture HIPing the fatigue life of electron beam melting (EBM) additively manufactured parts is currently dominated by the presence of porosity, exhibiting large amounts of scatter. Here we have shown that the size and location of these defects is crucial in determining the fatigue life of EBM Ti-6Al-4V samples. X-ray computed tomography has been used to characterise all the pores in fatigue samples prior to testing and to follow the initiation and growth of fatigue cracks. This shows that the initiation stage comprises a large fraction of life (>70%). In these samples the initiating defect was often some way from being the largest (merely within the top 35% of large defects). Using various ranking strategies including a range of parameters, we found that when the proximity to the surface and the pore aspect ratio were included the actual initiating defect was within the top 3% of defects ranked most harmful. This lays the basis for considering how the deposition parameters can be optimised to ensure that the distribution of pores is tailored to the distribution of applied stresses in additively manufactured parts to maximise the fatigue life for a given loading cycle.
url https://doi.org/10.1038/s41598-017-06504-5
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