The vibration bending fatigue life uncertainty of additively manufactured Titanium (Ti) 6Al-4V specimens is studied. In this investigation, an analysis of microscopic discrepancies between 10 fatigued specimens paired by stress amplitude is correlated to the bending fatigue life scatter. Through scanning electron microscope (SEM) analysis of fracture surfaces and grain structures, anomalies and distinctions such as voids and grain geometries are identified in each specimen. This data along with previously published results are used to support assessments regarding bending fatigue uncertainty. Corrections on stress and scatter based on microscopic features are implemented to the stress versus fatigue life comparisons. The results of this investigation show that the bending fatigue life uncertainty can be bounded by cold-rolled Ti 6Al-4V data when correcting the tested stress amplitude values with stress concentration effects and variation due to microstructure geometries. The understanding gained from this study is important for future development of a predictive vibration bending fatigue life model that will include the probability of geometry, density, and location of voids as an artifact of LPBF build parameters.
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ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition
June 11–15, 2018
Oslo, Norway
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5112-8
PROCEEDINGS PAPER
Investigating Discrepancies in Vibration Bending Fatigue Behavior of Additively Manufactured Titanium 6Al-4V
Onome Scott-Emuakpor,
Onome Scott-Emuakpor
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Casey Holycross,
Casey Holycross
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Tommy George,
Tommy George
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Luke Sheridan,
Luke Sheridan
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Emily Carper,
Emily Carper
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Joseph Beck
Joseph Beck
Perceptive Engineering Analytics LLC, Minneapolis, MN
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Onome Scott-Emuakpor
Air Force Research Laboratory, Wright-Patterson AFB, OH
Casey Holycross
Air Force Research Laboratory, Wright-Patterson AFB, OH
Tommy George
Air Force Research Laboratory, Wright-Patterson AFB, OH
Luke Sheridan
Air Force Research Laboratory, Wright-Patterson AFB, OH
Emily Carper
Air Force Research Laboratory, Wright-Patterson AFB, OH
Joseph Beck
Perceptive Engineering Analytics LLC, Minneapolis, MN
Paper No:
GT2018-75978, V006T24A015; 10 pages
Published Online:
August 30, 2018
Citation
Scott-Emuakpor, O, Holycross, C, George, T, Sheridan, L, Carper, E, & Beck, J. "Investigating Discrepancies in Vibration Bending Fatigue Behavior of Additively Manufactured Titanium 6Al-4V." Proceedings of the ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. Volume 6: Ceramics; Controls, Diagnostics, and Instrumentation; Education; Manufacturing Materials and Metallurgy. Oslo, Norway. June 11–15, 2018. V006T24A015. ASME. https://doi.org/10.1115/GT2018-75978
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