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Royal Belgian Institute of Marine EngineersTitanium Powder Metallurgy:A Review ‐ Part 1F.H. (Sam) Froes, FASM*Titanium and its alloys are the materialsof choice for many applications, but highcost often negates their use. Powdermetallurgy offers a cost‐effectivefabrication approach.Titanium alloys are among the most importantadvanced materials that are key to improvedperformance in aerospace and terrestrial systems [1‐5]due to their excellent combinations of specificmechanical properties (properties normalized bydensity) and outstanding corrosion behaviors [6‐10] .However, limiting widespread use of Ti alloys is theirhigh cost compared to competing materials. This hasled to numerous investigations of various potentiallylower‐cost processes [1‐3] including powder metallurgy(PM) techniques [1‐2,6‐10,12,13] This article discussestitanium PM technology including the blendedelemental (BE) approach, prealloyed (PA) methods,additive layer manufacturing (ALM), metal injectionmolding (MIM), and spray deposition (SD) processing.Not discussed are far‐from‐equilibrium processing(rapid solidification, mechanical alloying, and vapordeposition) and porous materials and powders forattaching to the surface of body implants. A morecomprehensive review of titanium PM will bepublished in 2013 [4] .The cost of fabricating various titanium precursorsand mill products has been discussed in severalpublications over the past few years [1‐3] ,noting thatthe cost of extraction is a small fraction of the totalcost of a component fabricated via the cast andwrought (ingot metallurgy) approach (Fig. 1). Toproduce a final component, the mill products shownin Fig. 1 must be machined, often with very high buy‐to‐fly ratios (which can reach as high as 40:1). Thegenerally accepted cost of machining a component isFig. 1 ‐ Cost of titanium at various stages of component fabrication.

that it doubles the cost of the component (with thebuy‐to‐fly ratio being another multiplier in cost perpound) as shown in Fig. 2. This means that anythingthat can be done to produce a component closer tothe final configuration will result in a cost reduction‐hence the attraction of near‐net‐shape PMcomponents.Titanium powder metallurgyTable 1 shows the characteristics of the differenttypes of titanium powders that are either available orunder development today. The table is based in parton a recent review of powder‐production methodscoauthored by McCracken [14] . The oxygen level ofthe hydride‐dehydride (HDH) powder can be reducedby deoxidizing with calcium[14] . It is also possible toconvert the angular HDH to a spherical morphologyusing the Telma process discussed later.Fig. 2 ‐ Boeing 787 side‐of‐body chord manufacturing cost breakdown.Courtesy of Boeing.Development of new titanium production methodssuch as the ITP / Armstrong, Fray, CSIRO(Commonwealth Scientific and Industrial ResearchOrganization, Australia), and MER processes shown inTable 1 is aimed at lowering the cost of PM titaniumpowder. However, these powders are not yetavailable, and their relative cost and processingcharacteristics are yet to be established.Companies/processes that produce prealloyedspherical titanium powder include: ATI Powder Metals, Pittsburgh, Pa. (formerlyCrucible Research Center); spherical gas‐atomizedalloy powder; 100‐lb capacity melting furnace. Advanced Specialty Metals, Nashua, N.H.; sphericalplasma rotating electrode process (PREP). Raymor Industries Inc., Boisbriand, Quebec, Canada(now includes Pyro genesis); spherical plasmaatomized. Baoji Orchid Titanium Industry Co. Ltd., China;spherical PREP. ALD Vacuum Technologies, Hanau, Germany;electrode induction melting gas atomized sphericalTi‐6Al‐4V powder. Sumitomo Sitex, Japan; gas atomized Ti‐6Al‐4Vpowder (0.08‐0.13 wt% oxygen). TLS Technik GmbH & Co., Bitterfeld, Germany; gasatomized. Affinity International; gas atomized and PREP (maybe out of business).‐Towa State University/ Ames Lab; experimental gasatomization; cost effective; very fine sphericalpowder ( 325 mesh, or 45 µm) produced using aclose‐coupled high pressure supersonic gas. Plans areto commercialize the process under a company calledIowa Powder Atomization Technologies. Tekna Induction, Sherbrooke, Quebec, Canada;plasma spheriodization process converts irregularshaped titanium powder (‐100/ 400 mesh, or ‐150/ 37 µm) to a spherical morphology of the samesize range, but with a significant improvement in tapdensity and flow rate. Quad Cities Manufacturing Laboratory, Rock Island,Ill.; plans to establish capabilities for PREP, gasatomization, HDH, and the Telma induction plasmaspheriodization process (to convert HDH powders).Atomized powders are generally prealloyed andspherical (Fig. 3a). Sponge fines (a byproduct ofsponge production) are angular, sponge‐like innature, and contain remnant salt, which preventsachievement of full density and adversely affectsweldability (Fig. 3b). Hydride‐dehydride powders,which are generally also prealloyed, are angular innature (Fig. 3c)[16] . Conversion to a sphericalmorphology using the Telma process is shown in Fig.3d.Nonmelt processesFour non‐melt processes appear to have the greatestpotential for scale‐up, with an additional processbeing developed by Advance Materials (ADMA)Products, Hudson, Ohio, which is also of potentialcommercial interest. The processes are the FFCCambridge approach, the MER technique, the (CSIRO)methods, and the ITP/Armstrong process. In the FFCCambridge approach, titanium metal is produced atthe cathode in an electrolyte (generally CaCl2) by theremoval of oxygen from the cathode. This techniqueallows the direct production of alloys such as Ti‐6Al‐4V at a cost that could be less than product of theconventional Kroll process[17] . The process is beingdeveloped by Metalysis in South Yorkshire, UK.The MER approach is an electrolytic method thatuses a composite anode of TiO2, a reducing agent,and an electrolyte, mixed with fused halides.Projections are for titanium production at asignificantly lower cost than the conventional Krollprocess [18] .

Fig. 3 ‐ (a) SEM photomicrograph of gas‐atomized prealloyed spherical Ti‐6Al‐4V (courtesy of Affinity International); (b) SEM photomicrograph ofsponge fines produced by the Kroll process (courtesy of Ametek); (c) SEM photomicrograph of angular HOH titanium powder; and (d) SEMphotomicrograph of spherical powder produced by processing angular HOH titanium to a spherical morphology using the Tekna technique.The CSIRO technique [19] builds upon the fact thatAustralia has some of the largest mineral and sanddeposits in the world. In this approach, cost‐effectivecommercially pure titanium is produced in acontinuous fluidized bed in which titaniumtetrachloride is reacted with molten magnesium (theTiRO process). They also have a proprietary processfor producing alloys (details unavailable at thepresent time). Continuous production of a wide rangeof alloys including aluminides and Ti‐6Al‐4V has beendemonstrated on a large laboratory scale. Thecommercially pure titanium powder produced wasused to fabricate extrusions, thin sheet by continuousroll consolidation, and cold‐spray complex shapesincluding ball valves and seamless tubing.Commercialization of the process is now in theplanning stage with a decision to proceed to the pilotplant stage likely to be taken in 2012.The ITP/ Armstrong method [1‐3] is continuous anduses molten sodium to reduce titanium tetrachloride,which is injected as a vapor. The resultant powderdoes not need further purification and can be useddirectly in the conventional ingot approach. Thepowder is most efficiently used in the powdermetallurgy technique. A range of alloys can beproduced (including the Ti‐6Al‐4V alloy) as a highquality homogeneous product suitable for manyapplications. ITP currently operates an R&D facility in2012, and will produce both commercially puretitanium and Ti‐6Al‐4V alloy powder.Fig. 5 ‐ The Toyota Altezza (1998 Japanese car of the year) is the firstfamily automobile in the world to feature titanium valves; Ti‐6Al‐4Vintake valve (left) and TiB/Ti‐Al‐Zr‐Sn‐Nb‐Mo‐Si exhaust valve (right).Courtesy of Toyota Central R&O Labs Inc.In the ADMA Products approach [20] , spongetitanium is cooled in a hydrogen atmosphere ratherthan the conventional inert gas. The hydrogenatedsponge is then easily crushed, and in thehydrogenated condition can be compacted to ahigher density than conventional low‐hydrogensponge; subsequent hydrogen removal is easilyaccomplished with a simple vacuum anneal. Theremnant chloride content of the hydrogenatedsponge is reported to be at low levels (helping toavoid porosity and enhancing weldability). There are14 patents covering this approach.Estimates of the powder shipments (annually in allcases) are HDH (1000‐2500 metric tons worldwideand 200‐400 metric tons U.S.) and spherical (150‐350metric tons worldwide and 20‐50 metric tons U.S.).Near‐net shapesFig. 4 ‐ Auto connecting rod fabricated via blended elemental approachusing hydrogenated titanium powder.Courtesy of Orest Ivasishin, Ukrainian Academy of SciencesLockport, III., and has broken ground on a fourmillion pound per year expansion in Ottawa, III.,which is expected to ramp up production throughoutTechniques generally available for production of nearnet shapes (NNS) are amenable for use with varioustypes of titanium powders; these includeconventional press‐and‐sinter, elastomeric bag coldisostatic pressing (CIP), and ceramic mold or metalcan hot isostatic pressing (HIP). Production of NNS isdivided into parts produced using blended elementalpowders and those produced using prealloyedpowders.The blended elemental approach is potentially thelowest cost titanium PM process, especially if anysecondary compaction step (e.g., HIP) can be avoided[15,21]. In the process, angular titanium sponge fines(or titanium hydride powder) and master alloycomposition (generally the 60 Al:40 V variety to

produce the Ti‐6Al‐4V composition) are blendedtogether, cold pressed, and sintered to near fulldensity. Use of titanium hydride enables achievingdensities very close to 100% in components such asthe auto connecting rod shown in Fig. 4, withmechanical properties at ingot‐metallurgy levels.Blended‐element PM technology using hydride‐dehydride (HDH) titanium powder produced by theKroll sponge process is the key to the commercialsuccess of Dynamet Technology Inc’.s (Burlington,Mass.) PM process [15] , which is producing a widerange of affordable PM mill products. Figure 5 showsvalves made using the BE process for productionmodels of the Toyota Altezza family automobile [1‐3] .Currently, ADMA Products' hydrogenated titaniumpowder manufacturing capacities are 50,000‐60,000lb/yr, and the company is installing a pilot scale unitthat will triple output [22] . Results of tests conductedby major aircraft companies and the U.S. DOE andDOD show that properties of the PM Ti alloys meetAMS specification and meet or exceed properties oftitanium wrought alloys made using conventionalingot‐metallurgy approaches.inert gas. The hydrogenated non Kroll powder wasused together with 60 Al:40 V master alloy toproduce components made of the Ti‐6Al‐4V alloy.Typical mechanical properties after cold pressing,sintering, forging, and annealing are shown in Table3. The mechanical properties compare well withthose exhibited by cast and wrought products. Thelow cost of the process in combination with theattractive mechanical properties make the approachwell suited to the cost‐obsessed automobile industry.A General Motors connection link weighing about0.705 lb (0.32 kg) was estimated to be less than 3.00[23].In the Kroll process, removal of Ti sponge from theretort and its subsequent crushing is time and energyintensive. In comparison, ADMA's process producesTiH2 that, unlike Ti sponge, is very friable and easilyremoved from retort with no need for an expensivesizing operation. ADMA's vacuum distillationprocessing time is also at least 80% less than in theKroll process, because phase transformations/latticeparameter changes of the hydride sponge in thepresence of hydrogen accelerate distillation removalof MgCl2. Finally, atomic hydrogen is released duringsintering‐dehydriding of TiH2 powder, and serves as ascavenger for impurities (e.g., oxygen, chlorine,magnesium, etc.) resulting in titanium alloys with lowinterstitials that at least meet properties of ingot‐metallurgy alloys, both static and S‐N fatiguebehavior [12] .Powders can be subsequently fabricated to otherproduct forms such as sheet. Alloy sheet can befabricated in a similar manner by adjusting the feedstock to a mixture of titanium powder and alloyingadditions.CHIP processDynamet Technology uses the CIP‐sinter or CHIP (CIP‐sinter‐HIP) process to produce NNS parts for finishmachining to high tolerance configurations andperforms [15] . The sintering process was historicallyestablished to reach a minimum density level atwhich the material had no interconnected porosity.At this density threshold, the material could be hotisostatically pressed without the processing expenseof HIP encapsulation, making it economically viable.Recent developments enabled achieving greater than98% sintered density, resulting in as‐sintered tensileproperties equivalent to those of wrought materialand superior to those of castings as shown in Table 2[15].This reduces the need for HIP and further strengthensthe economic advantage of PM CIP‐sintermanufacturing technology.Hydrogenated titanium processThe use of titanium hydride powder instead oftitanium sponge fines led to the achievement ofessentially 100% density in complex parts using asimple, cost‐effective press‐and‐sinter technique [20,21]. ADMA Products produced a lower cost titaniumhydride powder by cooling sponge produced in a Krollprocess with hydrogen rather than the conventional

References1. F.H. Froes, M.A. Imam, and Fray Derek, (editors), CostAffordable Titanium, TMS, Warrendale, Pa., 2004.2. M.N. Gungor, M.A. Imam, and F.H. Froes, (editors), Innovationsin Titanium Technology, TMS, Warrendale, Pa., 2007.3. M.A. Imam, F.H. Froes, and K.F. Dring, (editors), Cost‐Affordable Titanium III, TMS, Warrendale, Pa., 2010.4. F.H Froes, Powder Metallurgy of Titanium Alloys, Advances inPowder Metallurgy, Woodhead Publishing Ltd. Cambridge, UK, tobe published 2013.5. Materials Science and Engineering ‐ Forging Stronger Links toUsers, NMAB, National Academy Press pub NMAB‐492,Washington D.C., 1999.6. F.H. Froes, D. Eylon, and H. Bomberger (editors), TitaniumTechnology: Present Status and Future Trends, TDA, Dayton,Ohio, 1985.7. F.H. Froes, Yau Te‐Lin, and H.G. Weidenger, Titanium,Zirconium and Hafnium, Materials Science and Technology ‐Structure and Properties of Nonferrous Alloys, K.H. Matucha, VCHWeinheim, (editors), FRG, 401, 1996.8. F.H. Froes, Encyclopedia of Materials Science and Engineering,Elsevier, Oxford, UK, 2000.9. F.H. Froes, Titanium Alloys, Handbook of Advanced Materials,McGraw‐Hill Inc., New York, 2000.10. F.H. Froes, Titanium Metal Alloys, Handbook of ChemicalIndustry Economics, John Wiley and Sons Inc., New York, 2000.11. R.R. Boyer, G. Welsch, E.W. Collings (editors),Materials Properties Handbook: Titanium Alloys, ASM Intl.,Materials Park, Ohio, 1994.12. F.H. Froes and D. Eylon, Powder Metallurgy of TitaniumAlloys, Intl. Matls. Reviews, 35, 162, 1990.13. F.H. Froes and C. Suryanarayana, Powder Processing ofTitanium Alloys, Reviews in Particulate Materials, MPIF,Princeton, N.J., 1, 223, 1993.14. C. McCracken, Manufacture of hydride‐dehydride low oxygenTi‐6Al‐4V (Ti‐6‐4) powder incorporating a novel powder de‐oxidation step, Euro PM Conference, 2009.15. S.M. Abkowitz et al., Affordable PIM titanium ‐Microstructure, Properties and Products, MPIF Conference, 2011.16. C. McCracken, private communication, February 14, 2012.17. M. Bertolini, private communication, April 21, 2011.18. J. Withers, private communication, May 29, 2011.19. J.E. Barnes, private communication, November 7, 2011.20. G.I. Abakumov, V.A. Duz, and V.S. Maxson, Titanium alloymanufactured by low cost solid state PIM processes for military,aerospace and other critical applications, ITA Conference, 2010.21. F.H. Froes, et al., Cost Effective Synthesis of Ti‐6Al‐4V AlloyComponents Produced via the PIM Approach, Proc. TMSSymposium on High Performance Metallic Materials for CostSensitive Applications, Seattle, Wash., TMS, Warrendale, Pa.,2002.22. V.S. Maxson, private communication, October 17, 2011.23. V.S. Maxson, ADMA Corp., private com‐munication, October31, 2001.*Life Member of ASM international Tacoma, Wash.For more information: Dr. F.H. (Sam) Froes is a consultant, 5208Ridge Dr. NE, Tacoma, WA 98422;email: ssfroes @comcast.net.Source: ADVANCED MATERIALS & PROCESSES SEPTEMBER 2012

Titanium powder metallurgy Table 1 shows the characteristics of the different types of titanium powders that are either available or under development today. The table is based in part on a recent review of powder‐production methods coauthored by McCracken [14] . The oxygen level of

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