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Dr Dawie van Vuuren Mr Hardus Greyling
Titanium metal production and additive manufacturing – contributing to a vibrant new industry Dr Dawie van Vuuren Mr Hardus Greyling
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Outlay South Africa’s global Ti position South Africa’s Ti beneficiation strategy Primary Ti metal production Large area high speed additive manufacturing
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South African’s global Ti position in 2006
World Approximate Value Reserves 220 Mt TiO2 1300 Mt TiO2 Mineral Production 1090 kt TiO2 5200 kt TiO2 $ 175m p.a. $ 840 m.p.a. Slag Production $ 490m p.a. $ 2500 m.p.a. Pigment Production ~20 kt TiO2 5100 kt TiO2 $ 37m p.a. $ m.p.a. Sponge Production Nil 125 kt p.a. Ti $ 1250 m.p.a. Ingot Production 145 kt p.a. Ti $ 2600 m.p.a. Mill Products ~90 kt p.a. Ti $ 4500 m.p.a.
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Titanium Centre of Competence Supplier Development
Industrialisation & Commercialisation R&D Platforms Technology Development SA Ti Industry Supplier Development Design, Simulation and Modelling CSIR, ULim, Wits, NMMU Laboratories and R&D Facilities CSIR, NLC, SU, UCT, UP, NMMU, UJ, CUT, VUT, Wits, Mintek, Necsa Physical Metallurgy and Characterisation UCT, CSIR, UP, VUT Primary Metal Production CSIR Powder Consolidation SU UCT Investment Casting Friction Welding NMMU High Speed Additive Manufacturing CSIR, NLC Aerosud CUT High Performance Machining Fh IWU Sheet Forming Developing and commercialising Technology Building Blocks for the South African Titanium Industry Oil & Gas Marine Chemical Automotive Aerospace Medical 4
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Final Products/Components: USD/kg 150 – 20,000
Cheaper Titanium powder – Changing the industry Typical prices Ti Powder 10 USD/kg Ti Final Products/Components: USD/kg 150 – 20,000 Ti Powder 40 USD/kg Ti Ti Mill Products 50 USD/kg Ti Ti Ingot 20 USD/kg Ti Ti Sponge 10 USD/kg Ti Current SA industry TiCl4 4.4 USD/kg Ti TiO2 Pigment 5.3 USD/kg Ti TiO2 Slag 1.45 USD/kg Ti Ilmenite 1 USD/kg Ti
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Titanium Centre of Competence Primary Ti Production (CSIR Process)
Industrialisation plan for CSIR-Ti project 2011 2012 2013 2014 2016 2015 2017 2018 2021 2022 2020 2019 Titanium Centre of Competence Primary Ti Production (CSIR Process) STAGE 2: Basic Development STAGE 3: Pilot Phase (2kg/h) STAGE 4: Feasibility Phase STAGE 4 Implementation: Demonstration Plant 500 tpa Commercially Pure (CP) Ti STAGE 5: World-Class Plant: tpa CP Ti Completed R29m R m Concept design Cost estimate & feasibility Basic design Cost estimate & approval Detail design Construction Commissioning Operation R700m – R1bn CSIR Commercial partners
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CSIR-Ti pilot plant flow diagram
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CSIR-Ti process advantages
Continuous operation - 60 years after scaling up the batch Kroll process, there is still not a commercially proven continuous process. Economy of scale with lower capital and operating costs Downstream production and fabrication costs of titanium components are significantly less for Ti powder than for Ti sponge. CSIR-Ti process has lowest process temperature of all developments in the world that is currently being tested on a similar scale of operation. Scaling up is less risky with less corrosion, less salt entrapment, reduced reagent and by-product vapour pressures and less hazards. Closing of metal recycle loop much simpler than in other processes It is the only direct titanium powder production process that is currently being considered that gives the means to control Ti powder morphology.
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Panoramic view of CSIR-Ti pilot plant
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Additive Manufacturing (or “3D printing”)
Additive manufacturing (AM) is defined by ASTM as “the process of joining materials to make objects from 3D model data, usually layer upon layer, as opposed to subtractive manufacturing methodologies.” 10
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Additive Manufacturing (or “3D printing”)
Industries served AM used in final part production Source: Wohler report 2014 11
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Additive Manufacturing in aerospace
Manufacturing of high-value low-volume components Reduction of machining and processing time and material waste Manufacturing of parts in exotic materials Manufacturing of complex 3-D parts Manufacturing of assemblies Manufacturing of tools 12
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AM in the Aerospace industry
“Composite materials make up 50% of the primary structure of the 787 including the fuselage and wing” 13
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Additive Manufacturing
Ti beneficiation Billet Ingot Sponge Extensive Machining 90+% <5% Waste Ore Powder Min Machining Final Part Additive Manufacturing South African Development AeroSwift South African Capability 14
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Present limitations/opportunities
Limited production rate Inefficient laser manipulation Limited energy input Serial processing Limited part size High Cost Capital cost Production cost Material cost Aerospace Qualification 15
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Aeroswift - Objectives
Design and construct a large area, powder bed AM system, for metallic components: Powder layer manufacturing High speed system for Production of large metal parts High throughput Versatile to support optimisation of parameter field Build volume: 2m x 0.6m x 0.6m Scalable build volume Pre-heating and environmental control Materials that can be accommodated Ti-6Al-4V Stainless Steel alloys Inconel Other metals 16
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Laser Metals Deposition vs Selective Laser Melting
Characteristic Laser Metal Deposition (Direct Energy Deposition) Selective Laser Melting (Powder Bed Fusion) Materials Most metals, functionally graded builds Most metals Part size Depends on handling system 600mm x 500mm x 450 mm Aeroswift 2m x 620 mm x 620 mm Part complexity Limited Nearly unlimited Build rate mm3/sec Commercial systems mm3 sec, Aeroswift up to 60 mm3/sec Base Many geometries, also existing parts Flat plate Surface roughness (Rz) 60 to 100 µm 50 to 70 µm 17
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Aeroswift in the AM technology landscape
HIGHER VALUE Powder bed systems Part complexity Aeroswift Powder Deposition systems Wire deposition systems <500mm >2000mm Part size 18
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Aeroswift – Summary of 2014 Achievements
Phase 1: Machine design and construction completed Phase 2: Process development and optimisation started. (Nov 2014) Machine testing, evaluation and optimisation Parameter testing and optimisation Milestone: End 2017: Flight-ready demonstrator part Process development achievements Consolidation rates up to 60mm3 /sec demonstrated Low sample porosity (lower than 0.5%) Commercialisation strategy develop and presently being implemented 19
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Progress – Process development
Sample ¼ Charpy impact toughness at 25°C(J) Vickers Micro Hardness(HV) Ti6Al4V manufactured by 400W laser powder bed fusion machine 6 Milled and annealed reference sample 7-8 350 Ti6Al4V made by Aeroswift high power laser powder bed fusion technology 8-10 © CSIR 20
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Hardus Greyling Dr. Dawie v Vuuren
Thank you Questions? Hardus Greyling Dr. Dawie v Vuuren
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