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lion, while the cost of making the buckles using DMLS is

only $256,000.

The direct manufacturing ability of AM technologies

also helps reduce manufacturing costs in the case of high

buy-to-fly ratio parts. For example, researchers at Oak

Ridge National Laboratory built a Ti-6A-4V Bleed Air Leak

Detect (BALD) bracket for the Joint Strike Fighter (JSF)

engine using EBM technology (Fig. 10)

[14]

. Traditional man-

ufacturing from wrought Ti-6Al-4V plate costs almost

$1000/lb due to a high (33:1) buy-to-fly ratio as opposed to

just over 1:1 for the AM-built part. Estimated savings

through AM is approximately 50%.

Direct deposition techniques such as DMD can not

only be used to create parts, but these technologies can

also be used for remanufacturing, repair, and/or feature

building on existing parts. Damaged aerospace titanium

components such as bearing housings, flanges, fan

blades, casings, vanes, and landing gears can be rebuilt

using these technologies at 20-40% of the cost of new

parts[11]. Worn flanges in jet engine casings have been

rebuilt using DMD at less than half the cost of new

parts. Extensive work is also underway to investigate

the feasibility of using such technologies to salvage

components that are mismachined during conventional

manufacturing. Successful realization of these efforts

will have a significant impact on the titanium manufac-

turing industry. While most of the commercial activi-

ties in the AM industry are concentrated in the U.S. and

Europe, significant efforts are underway in other parts

of the world as well, including China

[15]

.

Conclusions

Significant advances in additive manufacturing tech-

nologies over the past few years have led to the production

of fully functional parts using titanium and its alloys. While

powder bed fusion technologies offer the ability to build

hollow near-net shapes with finer resolution, directed en-

ergy-based technologies offer the ability to add features to

existing parts and remanufacture and repair damaged

parts, besides building parts directly from CAD data. Most

studies reveal that the properties of AM material are as

good as, or superior to, conventionally fabricated titanium

alloys. Matching the correct AM technology to the appli-

cation, along with proper design optimization, can achieve

significant savings by reducing both weight and scrap. The

aerospace and medical industries have so far been the

largest users of titanium AMmaterials, while other indus-

tries, such as automotive, are beginning to exploit the ben-

efits of AM titanium alloys as well.

Acknowledgements

The authors recognize input for this article and useful discus-

sionswith JimSears, RyanDeHoff, RichardGrylls, JessicaNehro,

AndersHultman, ScottThompson, LauraKinkopf,MichaelClo-

ran, DavidWhittaker, Karl D’Ambrosio, andMa Quin.

For more information:

Bhaskar Dutta is Chief Operating

Officer at DM3D Technology LLC, 2350 Pontiac Rd.,

Auburn Hills, MI 48326, 248/409-7900,

bdutta@dm3dtech. com, www.dm3dtech.com

.

References

1. F.H. (Sam) Froes, Powder Metallurgy of TitaniumAlloys,

Advances in Powder Metallurgy.

Eds. Isaac Chang and

Yuyuan Zhao, Woodhead Publishing, Philadelphia, p 202,

2013.

2. Defense News,

p. 24, June 10, 2013.

3.

www.eos.info/additive_manufacturing/for_technology_ interested.

4.

www.arcam.com/technology/additive-manufacturing.

5.

www.dm3dtech.com/index.php/expertise-innovations/ experticeandinnovations-dmddtechnology.

6.

www.morristech.com/Docs/Ti64ELI%20DataSheet.pdf.

7. B. Dutta, et al.,

Adv. Mater. & Processes,

p 33-36, May 2011.

8. B. Dutta, et al., Rapid Manufacturing and Remanufac-

turing of DoD components Using Direct Metal Deposition,

9. The AMMTIAC Quarterly, Vol 6, No. 2, p 5-9, 2011.

10. Bhaskar Dutta, Harshad Natu, and Jyoti Mazumder, Near

net shape repair and remanufacturing of high value compo-

nents using DMD, TMS Proceedings, Vol 1: Fabrication, Ma-

terials, Processing and Properties, p 131-138, 2009.

11. Titanium Alloy Direct Deposited Products Ti-6Al-4V

Annealed. SAE Aerospace Material Specification (AMS)

4999A, Sept. 2009,

www.sae.org/technical/standards/ AMS4999A.

12. Private communication, DM3D Technology, July 2013.

www.optomec.com/Additive-Manufacturing-Technol- ogy/Laser-Additive-Manufacturing.

13.

www.manufacturingthefuture.co.uk/_resources/case- studies/TSB-AirlineBuckle.pdf.

14. Ryan Dehoff, et al.,

Adv. Mater. & Processes,

Vol 171,

No. 3, p 19-22, 2013.

15. Private communication, Ma Quin, July 2013.

ADVANCED MATERIALS & PROCESSES •

FEBRUARY 2014

23

Fig. 10 —

BALD bracket for Joint Strike Fighter (JSF) built using EBM

technology. Courtesy of ORNL.