POWDER METALLURGY AND SOLID STATE PROCESSING OF ARMSTRONG TITANIUM AND TITANIUM ALLOY POWDERS

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POWDER METALLURGY AND SOLID STATE PROCESSING OF ARMSTRONG TITANIUM AND TITANIUM ALLOY POWDERS William H. Peter (Bill), Craig A. Blue, Jim O. Kiggans, John D.K. Rivard* Oak Ridge National Laboratory, Oak Ridge, TN Charlie Yu, Clive Scorey*, Joe Capone, and John McKernon AMETEK Specialty Metal Products, Wallingford, CT Bill Ernst International Titanium Powder (ITP), Lockport, IL T. James Dorsch BAE Systems, Santa Clara, CA ITA Annual Conference 2007, Orlando, FL October 7-9 2007 * Formerly with Organization 1

Introduction Ti Offers Many Attractive Properties. High Specific Strength. Good Elevated Temperature Properties. Excellent Corrosion Resistance. Allows for Damage Tolerant Design. Cost and Availability Are a Concern Lead Times 12 to 18 Months Plate Prices of $35 to $50/Lb Cost Limits Application to Specific Markets. Critical Need for Basic Research into Lower Cost Refining and Processing New Low Cost Titanium Powders Could Initiate a Paradigm Shift in Titanium s Use in Industry Oak Ridge National Laboratory is Working with Industry to Develop the Necessary PM Technologies to Consolidate the New Low Cost Ti Powders Heat Exchangers http://www.titanmf.comtitanmf Land Combat Systems - Pegasus BAE Systems Biomedical - Knee Replacement 787 Boeing http://www.boeing.com/commercial/787family/index.html 2

Conventional Technology Compared to DARPA Funded Armstrong Process Kroll Process Armstrong (ITP) Process Mg Reduction of TiCl 4 Reduction of TiCl 4 in Na Liquid Loop Batch Process Continuous Process Requires Acid Leaching and Ability to Produce Prealloyed Powder Vacuum Arc Remelting Price of Powder Competitive with Kroll Finally Milled into Desired Product Sponge PM Approach Not Attractive PM Approach Economically Attractive Except for Specialty Components Thousands of Pounds of Powder Have Been Produced 3

International Titanium Powder (ITP), Armstrong Process Titanium Powder A 100 lb Drum of ITP Powder Received by ORNL New 4 Million Pound Titanium Plant Under Construction in IL, U.S. Chemical Analysis of Powder Has Fallen within Specification Grade 2 for CP Ti (e.g., 0.12 to 0.21 wt. % O) Grade 5 for Ti-6Al-4V Typical Powder Particle Size Range: 150 to 2000 µm Armstrong Titanium Powder with a mean size of 400 µm Morphology Energy Consumption for Reduction Process 50 Year Old Conventional Kroll Process = 355 MBtu/ton [Batelle-Columbus Laboratories,,(1975). Energy use patterns in metallurgical and non-metallurgical mineral processing] Armstrong Process = 165 MBtu/ton A 53.4% Reduction in Energy Consumption. Low Cost Powder Allows for: Near Net Shape Consolidation Compositing and Layered or Engineered Structures Ability to Use Beneficial Elements Not Possible in Conventional Processing (E.g., Small Additions of Boron )) International Titanium Powder 4 Million Pound Per Year Plant to be Finished in 2008 4

Processing Cost Break Down of Fabricating 1 Ti Plate ITP Low Cost Ti Powders Developed in DTi Program Address 25% of 1 Plate Fabrication Costs The Secondary Processing or Processing into Finished Product (62% VAR and Milling) Needs to Be Addressedd Conventional Milling Operations, Scrap Generated: 40 to 60% PM Approach with ITP Powder Ability to Reduce Scrap to Less Than 10% Cost Break Down to Produce 1 Thick Titanium Plate Using Kroll VAR Melted Titanium Hartman, A.D. et al. JOM September 1998. pp. 16-19 5

Development of Multiple PM Processes for Economical Product Near Net Shapes Hot Pressed, Forged, Press+Sinter Plate Forged, PIF, Hot Roll, HIP Bars and Rod Extrusion Low Cost Ti Powder Sheet Roll Compacted 6

Vacuum Hot Pressing (VHP) of ITP CP Ti and Ti-6Al 6Al-4V Plate and Near Net Shape Production VHP CP Ti Armstrong Ti and Ti-6Al-4V powder were vacuum hot pressed. Interstitial Levels of ITP CP Ti, VHP Produced Plate within Specification Mechanical testing, microstructures, and chemical analysis comparable to conventional wrought properties. Rivard, J.D.K. et al. JOM 57, 11, 2005. pp. 56-60 Sample ITP VHP CP Ti 900 C/30min VHP Ti-6Al-4V As VHP microstructures YS UTS Ductility [MPa] [MPa] [%] 517 617 20.7 CP Ti Grade 2 345 448 20.0 ITP VHP Ti-6Al-4V 950 C/60min 963 994 13.8 Ti-6Al-4V Grade 5 828 897 10.0 7

Fatigue Testing Procedure for VHP Ti-6Al-4V Plate Ti-6Al-4V ITP Powder Pressed at 1,050 o C, 1 hour in Vacuum Initial powder had slightly high oxygen compared to ASTM Grade 5 (O 2 ~ 023 0.23 wt. %). Consolidated Plate: O 2 ~ 0.25 wt. %, 200 ppm pickup p Hot Rolled VHP Plate (850 o C, 50% reduction) Round Bar Specimen with 1/8 testing diameter, less than half hot rolled gauge thickness R ratio,s min /s max = 01 0.1 Frequency = 10 Hz 8

Ongoing Fatigue Results Preliminary Results of Specimens Taken Normal to Rolling Direction Indicate ITP VHP Ti-6Al-4V Samples Are Comparable to Conventionally Pressed and Forged Powders 9

DTi Low-Cost Ti-6Al-4V Plates Show Comparable Ballistic Results to Conventional Wrought Plate Distribution Statement "A" (Approved for Public Release, Distribution Unlimited) VHP Consolidated Plate (950 o C and 1,050 o C) Ballistics testing performed at BAE Systems using MIL-DTL-46077G spec. 0.30 cal APM2 (same as 7.62mm AP). Velocity increased until 0.5 plate was penetrated. 1,050 o C Plate - Estimated V 50 ~2,037 fps, within 2% of conventional wrought Ti-6Al-4V properties for specific thickness of plate (ref: MIL-DTL-46077 spec). No cracking. Good deformation/ductility tilit (note: #4, Back). Extremely limited spalling. 950 o C Plate Estimated V50 >2,097 fps, within 0.3% of specification for specific plate thickness WITHOUT penetration. V50 test could not be completed due to insufficient test area. Low-cost Ti-6Al-4V plate exhibited comparable performance to wrought plate. Front and back of V 50 tested 1,050 o C VHP Ti-6Al-4V Plate 10

Development of Cold Isostatic Pressing / Pneumatic Isostatic Forging (CIP/PIF) Process Necessity for Cost Effective Method of Producing Plate and Near Net Shape Components PIF AMETEK Patented Process Rapid Gas Pressurization (1 to 2 Minutes) Very Preliminary CIP/PIF Work Performed with AMETEK Shows Promise Ballistic Results Have Been Comparable to Wrought Plate Mechanical Evaluation Ongoing Description VHP CIP/PIF VHP ITP Ti-6Al-4V CIP/PIF Tubes CIP/PIF Near Net Shape Stainless Steel Components CIP/PIF ITP Ti-6Al-4V % of Theoretical Density 99.4% 99.6% Oxygen Pickup 0.02 0.04 (wt. %) Microstructure Equiaxed Equiaxed Hardness (VHN) 343 +/- 31.9 346 +/- 27.3 VHP ITP Ti-6Al-4V CIP/PIF ITP Ti-6Al-4V 11

Ti Processing Extrusion Mechanical testing and microscopy ORNL, 1250 ton - extrusion press As-extruded Ti Extruded CP Ti Tensile Bars As-extruded Ti-6Al-4V Sample* YS [MPa] UTS [MPa] Ductility [%] Extruded Ti 407 552 17.0 Ti Grade 2 345 448 20.0 * Insufficient Ti-6Al-4V powder was available at the time of initial extrusion demonstration. Recent Increase in ITP Ti-6Al-4V powder production will enable ORNL to produce Ti-6Al-4V extrusions and test bars in the near future. 12

Roll Compaction of Armstrong (ITP) Derived Ti Powders Roll Compacted Rolls of Nickel Sheet Commercially Produced at AMETEK with over 50 years experience Collaborative Effort Between ORNL and AMETEK to Develop Roll Compaction Manufacturing Technology for Low Cost Titanium Powders Both Commercially Pure Ti and Ti-Al-V Alloys Have Been Roll Compacted ITP Powder Has Resulted in: Green Densities of 60 to 70% Sheet Widths of 15 (or Greater) and Proof of Continuous Production (Coils of 28 in length) Solid State Sheet Processing After Roll Compaction: Sinter, Cold Roll, And Anneal Lead to Fully Consolidated Sheet (>99%) Initial Trial Resulted in High Strength/Low Ductility Due to High Oxygen However, Further Development Has Led to Acceptable Oxygen Levels: 200ppm Pickup or Less During Roll Compaction, and Less Than 800ppm Pickup After Full Consolidation Mechanical Testing Ongoing Distribution Statement A (Approved for Public Release, Distribution Unlimited) Diagram of Roll Compaction Sheet Production with AMETEK Roll Compaction Mill Roll Compacted Titanium Sheet 13

Results of ITP Ti Press+Sinter ITP Ti-6Al-4V Press+ Sinter Samples with Microstructure ITP CP Ti and Ti-6Al-4V Powders Pressed to Pressures of 100 ksi Sintered at Temperatures 1,100 o C and 1,300 o C Densities for given loads and temperatures: Up to 90% theoretical for CP Ti Up to 95% theoretical for ITP Ti-6Al-4V < 300 to 400 ppm pickup in oxygen Further Work in Progress Low Cost Ti Green Near Net Shape Component 14

Conclusions Low Cost Titanium Powders Are Now Produced That Could Cause a Paradigm Shift in the Use of Titanium i for Industry and Other Applications. Further Development in Solid State Consolidation of the New Titanium Powders Is Required to Realize the Most Economical Components and Penetrate New Markets. Vacuum Hot Pressed Plates and Extruded Bar of the Low Cost Titanium Have Been Produced with Tensile Properties that Meet ASTM Specifications. Very Preliminary Ballistic and Fatigue Results are Encouraging. Future Work Further Development of Existing Work Shown Comprehensive Mechanical Testing for Various PM Approaches (CP Ti, Ti-6Al-4V) PM Development of Other Low Cost Powders as Made Available Currently Fabricating 200lb Military Component from ITP Powders Welcome Any Further Collaboration to Allow for the Penetration of Titanium Into New Markets Heat Treatment and Rolling of Ti-6Al-4V Plates for 200lb Military Component 15

Acknowledgements The Research Presented Was Made Possible by the Support of: Department of Energy, Office of Energy Efficiency and Renewable Energy, Industrial Technologies Program (DOE- EERE-ITP Department of Energy, Office of Energy Efficiency and Renewable Energy, FreedomCar & Vehicle Technologies Program- Weight Reduction of Heavy Vehicles Program (DOE- EERE-FreedomCAR) Defense Advanced Research Programs Agency (DARPA), Defense Science Office (DSO), DARPA s Initiative in Titanium Program (DTi) I would like to thank the following individuals: Oak Ridge National Laboratory, Phil Sklad, Evan Ohriner, Steve Nunn, David Harper, Donny McInturff, Ed Hatfield, and Kevin Harper International Titanium Powder, Stanley S. Borys, Lance Jacobsen, and Dariusz Kogut AMETEK, Joe Capone, Greg Nelson Taras Lyssenko Questions? 16