Electron beam melting (EBM) additive manufacturing (AM) technology has allowed the layerwise fabrication of parts from metal powder precursor materials that are selectively melted using an electron beam. An advantage of EBM technology over conventional manufacturing processes has been the capability to change processing variables (e.g., beam current, beam speed, and beam focus) throughout part fabrication, enabling the processing of a wide variety of materials. In this research, additional scans were implemented in an attempt to promote grain coarsening through the added thermal energy. It is hypothesized that the additional energy caused coarsening of Ti-6Al-4V microstructure that has been shown to increase mechanical properties of as-fabricated parts as well as improve surface characteristics (e.g., reduced porosity). Fatigue testing was performed on an L-bracket using a loading configuration designed to cause failure at the corner (i.e., intersection of the two members) of the bracket. Results showed 22% fatigue life improvement from L-brackets with as-fabricated conditions to L-brackets with a graded microstructure resulting from the selective addition of thermal energy in the expected failure region. Three L-brackets were fabricated and exposed to a triple melt cycle (compared to the standard single melt cycle) during fabrication, machined to specific dimensions, and tested. Results for fatigue performance were within ∼1% of wrought L-brackets. The work from this research shows that new design procedures can be implemented for AM technologies that involve evaluation of stress concentration sites using finite element analysis and implementation of scanning strategies during fabrication that help improve performance by spatially adjusting thermal energy at potential failure sites or high stress regions.

References

1.
Murr
,
L. E.
,
Esquivel
,
E. V.
,
Quinones
,
S. A.
,
Gaytan
,
S. M.
,
Lopez
,
M. I.
,
Martinez
,
E. Y.
,
Medina
,
F.
,
Hernandez
,
D. H.
,
Martinez
,
E.
,
Martinez
,
J. L.
,
Stafford
,
S. W.
, and
Wicker
,
R. B.
,
2009
, “
Microstructures and Mechanical Properties of Electron Beam-Rapid Manufactured Ti-6Al-4V Biomedical Prototypes Compared to Wrought Ti-6Al-4V
,”
Mater. Charact.
,
60
(
2
), pp.
96
105
.
2.
Yoder
,
G. R.
,
Cooley
,
L. A.
, and
Crooker
,
T. W.
,
1977
, “
Observations on Microstructurally Sensitive Fatigue Crack Growth in a Widmanstatten Ti-6Al-4V Alloy
,”
Metall. Trans. A
,
8
(11), pp.
1737
1743
.
3.
Nalla
,
R. K.
,
Boyce
,
B. L.
,
Campbell
,
J. P.
,
Peters
,
J. O.
, and
Ritchie
,
R. O.
,
2002
, “
Influence of Microstructure on High-Cycle Fatigue of Ti-6Al-4V: Bimodal vs. Lamellar Structures
,”
Metall. Mater. Trans.
,
33
(3), pp.
899
918
.
4.
Bantounas
,
I.
,
Lindley
,
T. C.
,
Rugg
,
D.
, and
Dye
,
D.
,
2007
, “
Effect of Microtexture on Fatigue Cracking in Ti-6Al-4V
,”
Acta Mater.
,
55
(
16
), pp.
5655
5665
.
5.
Benedetti
,
M.
,
Heidmann
,
J.
,
Peters
,
J. O.
, and
Lutjering
,
G.
,
2005
, “
Influence of Sharp Microstructural Gradients on the Fatigue Crack Growth Resistance of α+β and Near-α Titanium Alloys
,”
Fatigue Fract. Eng. Mater. Struct.
,
28
(10), pp.
909
922
.
6.
Gil
,
F. J.
, and
Planell
,
J. A.
,
2000
, “
Behaviour of Normal Grain Growth Kinetics in Single Phase Titanium and Titanium Alloys
,”
Mater. Sci. Eng.
,
283
(1–2), pp.
17
24
.
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