Support Structures Remedies Reduce need for supports by reducing residual stresses as part is built, (e.g. better process control, scanning strategies etc.) More intelligent supporting algorithms to reduce unnecessary supports Modify part design to require fewer supports Modelling of SLM process Thermo-mechanical FEA model of SLM process taking into account changes of state. Interfaced with script that provides input to model based on process parameters. Being used to investigate effect of scanning strategies on residual stress and microstructure development. Acknowledgment: Luke Parry, PhD student 1 Support Structures: Design rules for SLM Vandenbroucke & Kruth (2007) Sutcliffe et al. (2005) Brooks et al. (2007) Mercelis & Kruth (2006) Thomas (2009) Varying design guidelines for different machines Some angle limit Horizontal overhang distance Automated tool under development to modify geometry to reduce support amount. 2 Automated tool to modify geometry Modify part design to require fewer supports as pre-build processing step Multiobjective optimisation to find best build orientation that: 1. 2. 3. Minimises modification required to geometry to self-support in regions where geometry modifiers are to remain as part of the part Minimises supports in regions where they will be removed Minimises build height (build time) Downward facing edges / faces categorised based on violation of self-support and line-of-sight conditions (tool access) 3 Automated tool to modify geometry Truss approach to geometry modifier, rather than filling +/- angled modifier geometry Iterative generation of self-supporting geometries Act as pre-build geometry filter Re-optimisation of geometry to compensate for additional material 4 Enclosed Voids 5 Enclosed Voids Draw direction constraint Increase in mass of 17% 6 Small minimum feature size Efficient mesh improvement and analysis techniques Example of octree decomposition with topology optimisation Using high maximum element dimension and high adjacency rule 7 Ongoing metal AM design projects ALSAM Project Application: ALSAM (Aluminium Lattice Structures via AM) Funded by the UK’s innovation agency, the Technology Strategy Board With: Develop and integrate technologies: SLM of aluminium alloy Lattice generation analysis and optimisation methods Efficient analysis and optimisation techniques are required for lattice structures which are highly complex geometrically. 9 ASID Project Application: ASID (Advanced Structural Integrated Demonstrator) Funded by the UK’s innovation agency, the Technology Strategy Board (Highly Innovative Technology Enablers for Aerospace 2 (HITEA2) call) With BAE Systems & Advanced Manufacturing Research Centre (AMRC), Sheffield Develop & integrate technologies: Thermoplastic composite structure. Additive Manufacturing of topologically optimised Titanium hinges. Fastener-less joining of Titanium to composite joints. Assess potential to: Improve current design philosophy Reduce overall manufacturing cost and life cycle maintenance requirements Courtesy of Need suitable design methods to allow application to practical components to be built using SLM. 10 INNOVATE Project Application: INNOVATE (Integration of Novel Aircraft Technology) Moving towards a More Electric Aircraft Reduce fuel consumption: for high power-density electrical machinery. Aim: To show that the design freedom offered by AM is the key for the 3D optimisation of machines Objective: Modelling and optimisation of brushless electrical motors with thermodynamics and electromechanics considerations heat dissipation (novel heat-sink design) electromechanical performance (novel rotor and stator designs) 11 ALMER Project Application: ALMER (Advanced Laser-additive-layer Manufacture for Emissions Reduction) Funded by the UK’s innovation agency, the Technology Strategy Board (Highly Innovative Technology Enablers for Aerospace 2 (HITEA2) call) With Rolls Royce, Materials Solutions, and The Manufacturing Technology Centre, Coventry Tackle manufacturing challenges so that potential design opportunities afforded by AM can be exploited fully. Multi-disciplinary thermo-mechanical model to predict residual stress during SLM build. Investigate the use of lattice structures for controlling residual stresses. Integrate model into design & optimisation tool to exploit the weight reduction opportunities in component design and minimise processing difficulties. 12 Design for Multifunctional AM Multifunctional 3D Printing Centre Vision: To take AM beyond geometry and single materials to the “printing” of multifunctional, multi-material components / devices / systems in one operation. Jetting process focused Volume based geometric modelling Further design freedom and complexity added to the design process Handling of interaction between cost, mechanical, electrical, thermal etc. to determine overall optimal solution Complex modelling and optimisation task More info at: www.nottingham.ac.uk/research/groups/3dprg 14 www.3dp-research.com Example Parts Applied industrial part Optimised Topology Component placement (based on geometric features and performance analysis) Routing optimisation (fixed and flexible order components) 3D routed connections Internal component placed and oriented More info at: An optimization based design framework for multifunctional 3D printing, (Brackett, Panesar, Ashcroft, Wildman, Hague) 15 Example Parts Anthropomorphic arm Representation with integrated sensors and conductive paths built using jetting. Showpiece by summer intern students for Science Museum exhibition: 3D Printing the Future. Ongoing further work by final year project undergraduate students to optimise the design using developed placement and routing techniques. 16 Summary Need new design tools to maximise potential of AM Need to include the manufacturing constraints of AM into tools Lattices / Cellular structures Topology optimisation Tools to accommodate manufacturing constraints Simulation of manufacturing process to allow better design Tools for volume based design (multi-material) 17 Conference Monday 7th - Friday 11th July, 2014 @ The Nottingham Belfry Hotel Monday 7th July (am) Introduction to AM & 3DP Master Class (pm) Overview of research activities in UK Universities Tuesday 8th & Wednesday 9th July 9th International Conference on AM & 3DP Wednesday 9th & Thursday 10th July ASTM F42 International Standards Group meeting Thursday 10th & Friday 11th July ISO/TC 261 Standards Meeting More info at: www.am-conference.com 18 Dr. David Brackett Faculty of Engineering, The University of Nottingham, University Park, Nottingham, NG7 2RD, UK Tel: +44 (0) 115 84 68441 Email: david.brackett@nottingham.ac.uk Web: www.3dp-research.com www.nottingham.ac.uk/3dprg