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Projects: Projects for Investigator
Reference Number EP/M021963/1
Title Virtual Testing of Additively-Manufactured Hybrid Metal-Composite Structures
Status Completed
Energy Categories Renewable Energy Sources(Ocean Energy) 5%;
Renewable Energy Sources(Wind Energy) 5%;
Not Energy Related 90%;
Research Types Basic and strategic applied research 100%
Science and Technology Fields PHYSICAL SCIENCES AND MATHEMATICS (Metallurgy and Materials) 50%;
ENGINEERING AND TECHNOLOGY (Mechanical, Aeronautical and Manufacturing Engineering) 50%;
UKERC Cross Cutting Characterisation Not Cross-cutting 100%
Principal Investigator Dr LF Kawashita
No email address given
Aerospace Engineering
University of Bristol
Award Type Standard
Funding Source EPSRC
Start Date 01 January 2016
End Date 30 June 2017
Duration 18 months
Total Grant Value £99,084
Industrial Sectors Aerospace; Defence and Marine; Manufacturing
Region South West
Programme Manufacturing: Engineering
 
Investigators Principal Investigator Dr LF Kawashita , Aerospace Engineering, University of Bristol (100.000%)
  Industrial Collaborator Project Contact , University of Bristol (0.000%)
Project Contact , Renishaw PLC (Old Town) (0.000%)
Project Contact , TEUFELBERGER Ges.m.b.H.., Austria (0.000%)
Web Site
Objectives
Abstract Additive Layer Manufacturing (ALM) has the potential to revolutionise the design and manufacture of hybrid joints by enabling tailored metal-composite interfaces that promote the optimal load transfer between metal and fibres. This will enable high-performance / high-endurance hybrid structures which can be manufactured via 'co-curing' processes, i.e. consolidation in a single step without the need for secondary adhesive bonding. However, in order to achieve optimal designs a high-fidelity modelling strategy is necessary.This project will develop and validate modelling strategies to:1. Predict the detailed meso-scale structure of hybrid metal-composite materials after manufacture and consolidation, including local fibre orientation with respect to metallic surface protrusions. These methodologies will be validated against micro-CT scans of real specimens.2. Resolve stresses at the level of individual tows/yarns and protrusions, accounting for thermal residual stresses and stresses due to externally applied loads. These data will provide an initial measure of the quality results can be used in the development of load path-based optimisation at the micro- or meso-scale levels3. Analyse joint strength and damage/fracture propagation properties due to combinations of quasi-static, impact and cyclic loading. Validate the methodologies against mechanical tests on real specimens.In a broader sense, this research introduces two new concepts for the design of hybrid metal-composite structures, namely:1. Performance-driven design, with performance being evaluated at the level of individual material constituents (i.e. fibres, matrices and metals), considering realistic micro-structures obtained via in-depth knowledge of the manufacturing process.2. Enabling the optimisation of damage tolerant designs where the objective measure of performance is related to both damage initiation and evolution. Due to time and resource constraints this First Grant research will enable the development of the virtual testing capability only, while the development of a closed-loop optimisation technique will be the focus of future work.
Publications (none)
Final Report (none)
Added to Database 28/03/19