EPSRC logo

Details of Grant 

EPSRC Reference: EP/D056276/1
Title: Coupling between Strain Induced Damage, the Degradation of Thermal Properties and Stress-Strain Response of Ceramic Matrix Composites
Principal Investigator: Hayhurst, Professor DR
Other Investigators:
Sheikh, Dr MA
Researcher Co-Investigators:
Project Partners:
Alstom Group Goodrich Hitco Carbon Composites, Inc.
Rockwell Rolls-Royce Plc University of California Santa Barbara
Department: Mechanical Aerospace and Civil Eng
Organisation: University of Manchester, The
Scheme: Standard Research (Pre-FEC)
Starts: 01 January 2007 Ends: 30 April 2010 Value (£): 288,575
EPSRC Research Topic Classifications:
Materials Characterisation Materials testing & eng.
Numerical Analysis
EPSRC Industrial Sector Classifications:
Aerospace, Defence and Marine
Related Grants:
Panel History:  
Summary on Grant Application Form
Funds are sought to employ a Research Assistant and a Research Student to research the modelling of the coupling between manufacturing porosity/damage, strain-induced damage, the degradation of thermal properties and stress-strain response of woven Ceramic Matrix Composites (CMCs). The project is a continuation of research done on GR/K81256, and on subsequent projects.Two CMC materials have been selected. The first is a simple plain 0/90 weave DRL-XT C/SiC CMC which has previously been studied extensively. The material will be researched using classical Finite Element unit cell modelling techniques to establish methods for modelling the coupling of manufacturing porosity and strain-induced damage with the degradation of thermal conductivity. The modelling will take place at the level of the fibre/tow/matrices materials, with the driver being to predict bulk composite properties from the physical and mechanicl properties of the constituent phases of the composite i.e. fibres, tows of fibres, interfaces between different materials and the matrices which hold the composite together.The next part of the research will be to repeat this modelling exercise on the DRL-XT C/SiC with the more computationally economic and conceptually simple Binary Modelling technique; with a view to establishing its viability and accuracy.Having established this, the Binary Modelling technique used on the first material, will be used to study the second one. That is a more complex HITCO C/C 8-Satin weave which is extensively used in industrial engineering components. The coupling between manufacturing porosity, strain-induced damage and the degradation of the thermal properties of the 8-Satin CMC will be researched. For both materials, success of the computer modelling will be judged against experimental stress-strain-thermal conductivity data collected under grant GR/K81256.The research will establish mehodologies for characterisation of manufacturing porosity, for eliciting physical and mechanical properties of fibres, tows, interfaces and matrices, using semi-inverse techniques and bulk composite experimental data.Lastly, the Binary Modelling technique will be used to predict the stress-strain-damage-thermal transport response of a simple engineering component subjected to combined thermal and mechanical loading; and to assess the viability of the approach. Recommendations will be made on viability and possible constraints to use for thermo-mechanical modelling e.g. complex woven composites.
Key Findings
This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
Potential use in non-academic contexts
This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
Impacts
Description This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
Summary
Date Materialised
Sectors submitted by the Researcher
This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
Project URL:  
Further Information:  
Organisation Website: http://www.man.ac.uk