Strain-Controlled High-Temperature (400°C) Low-Cycle Fatigue of Additive Manufactured Ti6Al4V Alloy

<div>The tensile and low-cycle fatigue (LCF) properties of Ti6Al4V specimens, manufactured using the selective laser melting (SLM) additive manufacturing (AM) process and subsequently heat-treated in argon, were investigated at elevated temperatures. Specifically, fully reversed strain-controlled tests were performed at 400°C to determine the strain-life response of the material over a range of strain amplitudes of industrial interest. Fatigue test results from this work are compared to those found in the literature for both AM and wrought Ti6Al4V. The LCF response of the material tested here is in-family with the AM data found in the literature. Scanning electron microscopy performed on the fracture surfaces indicate a marked increase in secondary cracking (crack branching) as a function of increased plastic deformation and demonstrating equivalent performance when compared to the wrought Ti6AL4V at RT (room temperature) at 1.4% strain amplitude and better performance when compared to the HIP-AM Ti6Al4V at RT.</div>

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Publication Details

Journal
SAE International Journal of Materials and Manufacturing
Published
2025-03-21
DOI
https://doi.org/10.4271/05-18-03-0024
Primary Topic
Additive Manufacturing Materials and Processes
Type
article
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article

Strain-Controlled High-Temperature (400°C) Low-Cycle Fatigue of Additive Manufactured Ti6Al4V Alloy

Robert L. Amaro, Narendra Kumar Gadwal, Mark E. Barkey, Zach Hagan et al.
1 links
SAE International Journal of Materials and Manufacturing
Additive Manufacturing Materials and Processes
article

Strain-Controlled High-Temperature (400°C) Low-Cycle Fatigue of Additive Manufactured Ti6Al4V Alloy

Robert L. Amaro, Narendra Kumar Gadwal, Mark E. Barkey, Zach Hagan, Jason G. McDuffie
article en

Abstract

<div>The tensile and low-cycle fatigue (LCF) properties of Ti6Al4V specimens, manufactured using the selective laser melting (SLM) additive manufacturing (AM) process and subsequently heat-treated in argon, were investigated at elevated temperatures. Specifically, fully reversed strain-controlled tests were performed at 400°C to determine the strain-life response of the material over a range of strain amplitudes of industrial interest. Fatigue test results from this work are compared to those found in the literature for both AM and wrought Ti6Al4V. The LCF response of the material tested here is in-family with the AM data found in the literature. Scanning electron microscopy performed on the fracture surfaces indicate a marked increase in secondary cracking (crack branching) as a function of increased plastic deformation and demonstrating equivalent performance when compared to the wrought Ti6AL4V at RT (room temperature) at 1.4% strain amplitude and better performance when compared to the HIP-AM Ti6Al4V at RT.</div>

SAE International Journal of Materials and ManufacturingVol. 18(3)
University of Alabama (US), Starmet Corporation (United States) (US), Advanced Materials Technology (United States) (US)
Openalex Percentile: Top 95%
Additive Manufacturing Materials and Processes
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Strain-Controlled High-Temperature (400°C) Low-Cycle Fatigue of Additive Manufactured Ti6Al4V Alloy — Robert L. Amaro, Narendra Kumar Gadwal, et al. · SAE International Journal of Materials and Manufacturing (2025) | TGRS Research Map | TGRS