Advanced Ceramic Matrix Composites for Energy Generating Gas Turbine Applications

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Title
Advanced Ceramic Matrix Composites for Energy Generating Gas Turbine Applications

CoPED ID
6b6765f5-a09f-4709-b130-e634327fa9d1

Status
Closed


Value
£791,192

Start Date
Sept. 30, 2008

End Date
Sept. 29, 2012

Description

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The purpose of this project is to develop the technology required for the implementation of an oxide/oxide ceramic matrix composite (CMC) in gas turbine applications. The ability to use oxide/oxide CMC’s for components in the combustor and turbine of the gas turbine would provide a step change in component temperature capability, enabling higher operating temperatures, improved engine efficiency and reduced CO2 emissions relative to the nickel based alloys currently used in these applications.
CMCs that offer these capabilities are being developed outside of the UK, but these materials are expensive and export controls or competitive barriers exist for the materials and/or the key enabling technologies required for their implementation. Therefore, developing a UK capability for the manufacture and implementation of a high temperature CMC, as undertaken in this programme, offers significant technical and financial benefits for high tech industries operating from within the UK.
To address the requirements for a material with a higher temperature capability than the nickel-based superalloys, an oxide/oxide CMC previously developed by Birmingham University (UoB) using a novel process route, that offers considerable benefits over the current technology, will be further developed within the programme and the technology transitioned from the laboratory environment to one of the industrial partners for adaptation and scaling of the process. Other elements of the programme include the manufacture of laminates and sub-elements in the CMC; the development of a thermal/abradable coating for the CMC; the characterisation of the material in terms of its physical and mechanical properties and failure/degredation mechanisms; assessment of non-destructive evaluation (NDE) techniques for examining the laminates and sub-elements; the development of a lifing methodology for oxide/oxide CMC’s; a review of potential repair techniques for CMCs and their coatings; and sub-element validation testing to prove the efficacy of the manufacturing processes, design concepts and lifing methods established during the programme.

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Subjects by relevance
  1. Technological development
  2. Emissions
  3. Gas turbines
  4. Development programmes
  5. Composites

Extracted key phrases
  1. Energy Generating Gas Turbine Applications
  2. Advanced Ceramic Matrix Composites
  3. Oxide CMC
  4. Oxide ceramic matrix composite
  5. High temperature capability
  6. High temperature cmc
  7. Component temperature capability
  8. High operating temperature
  9. Gas turbine application
  10. UK capability
  11. High tech industry
  12. Current technology
  13. Element validation testing
  14. Purpose
  15. Novel process route

Related Pages

UKRI project entry

UK Project Locations