Advanced ceramic matrix composites for energy generating gas turbine applications

Lead Research Organisation: University of Birmingham
Department Name: Metallurgy and Materials

Abstract

The project will develop a high temperature oxide/oxide ceramic matrix composite (CMC) for use in power generating gas turbine applications. This will provide a step change in temperature capability enabling higher operating temperatures, improving engine efficiency and reducing CO2 emissions. To achieve these objectives development of a CMC manufactured by a novel processing route is proposed. The programme will generate a fundamental understanding of the material, its failure/degradation mechanisms, optimised manufacturing process, NDE lifing, and repair issues. The academic partners will provide the CMC technology and the materials understanding. Industry will develop the NDE, lifing technologies, scale the process up to pilot plant level and provide the exploitation route.

Publications

10 25 50
 
Description A method of manufacturing for a ceramic matrix composite oxide-oxide system has been developed
Exploitation Route Technology can be exploited in transportation more generally.
Sectors Aerospace, Defence and Marine,Energy,Transport

 
Description Oxide- oxide ceramic matrix composites have been manufactured including a thermal protection system. If this becomes a favoured technology for Rolls-Royce plc the know how has been captured.
First Year Of Impact 2013
Sector Aerospace, Defence and Marine
Impact Types Economic

 
Description ATI
Amount £16,000,000 (GBP)
Funding ID TS/P00198X/1 
Organisation Innovate UK 
Sector Public
Country United Kingdom
Start 09/2016 
End 02/2020
 
Description EPSRC Programme Grant
Amount £2,000,000 (GBP)
Funding ID EP/P00878/1 
Organisation Engineering and Physical Sciences Research Council (EPSRC) 
Sector Public
Country United Kingdom
Start 09/2016 
End 08/2020
 
Title METHOD OF MANUFACTURING A CERAMIC MATRIX COMPOSITE ARTICLE 
Description A method of manufacturing a ceramic matrix composite article comprising the steps of: — a) forming a slurry consisting of water, polyvinyl alcohol, nitric acid, polyethylene glycol and alumina particles only, b) providing a length of fabric, the fabric comprising a plurality of ceramic fibres, c) applying slurry to at least one of the sides of the length of fabric such that the slurry adheres and impregnates the length of fabric, d) drying the slurry impregnated length of fabric, e) cutting the slurry impregnated length of fabric into a plurality of pieces of slurry impregnated laminates of fabric, f) applying water to each of the pieces of slurry impregnated laminates of fabric to reactivate the slurry, g) stacking the plurality of pieces of slurry impregnated laminates of fabric on a first mould part, h) consolidating the plurality of pieces of slurry impregnated laminates of fabric on the mould part, and i) sintering the stack of the plurality of pieces of slurry impregnated laminates of fabric to form an alumina matrix composite article. 
IP Reference US2011259506 
Protection Patent granted
Year Protection Granted 2011
Licensed Commercial In Confidence
Impact None