Investigating Discrepancies in Vibration Bending Fatigue Behavior of Additively Manufactured Titanium 6Al-4V

Author:

Scott-Emuakpor Onome1,Holycross Casey2,George Tommy2,Sheridan Luke2,Carper Emily2,Beck Joseph3

Affiliation:

1. Mem. ASME Air Force Research Laboratory, Aerospace Systems Directorate, Wright-Patterson AFB, OH 45433 e-mails: ;

2. Mem. ASME Air Force Research Laboratory, Aerospace Systems Directorate, Wright-Patterson AFB, OH 45433 e-mail:

3. Mem. ASME Perceptive Engineering Analytics, LLC, Minneapolis, MN 55418 e-mail:

Abstract

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 ten fatigued specimens paired by stress amplitude is correlated with 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. These data along with previously published results are used to support assessments regarding bending fatigue uncertainty. The understanding gained from this study is important for the future development of a predictive vibration bending fatigue life model.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

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