Fatigue and Strength Studies of Titanium 6Al–4V Fabricated by Direct Metal Laser Sintering

Author:

Scott-Emuakpor Onome1,Holycross Casey1,George Tommy1,Knapp Kevin2,Beck Joseph3

Affiliation:

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

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

3. Mem. ASME Perceptive Engineering Analytics, Lino Lakes, MN 55014 e-mail:

Abstract

Vibratory bending fatigue behavior of titanium 6Al–4V plate specimens manufactured via direct metal laser sintering (DMLS), powder bed fusion additive manufacturing (AM), is assessed. Motivation for the work is based on unprecedented performance demands for sixth-generation gas turbine engine technology that requires complex, lightweight components. Due to cost, schedule, and feasibility limitations associated with conventional manufacturing, AM aims to address ubiquitous component concepts. Though AM has promise in the engine community, process controls necessary for consistent material properties remain an enigma. The following manuscript compares variability of DMLS fatigue and strength to cold-rolled data. Results show discrepancies between DMLS and cold-rolled for fatigue and microstructure characteristics.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference30 articles.

1. Global Horizons Final Report, United States Air Force Global Science and Technology Vision,2013

2. Engine Structural Integrity Program (ENSIP),2002

3. Rapid Manufacturing With Direct Metal Laser;“,2002

4. Additive Manufacturing—Direct Laser Sintering of Titanium and Other Metals

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