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UK funding (£6,302,733): SILOET II Project 19, CMC and High Temperature Technologies Ukri 1 Jan 2014 UK Research and Innovation, United Kingdom

Overview

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SILOET II Project 19, CMC and High Temperature Technologies

Abstract Future civil aerospace gas turbine competitiveness will rely on higher temperature core turbo machinery and higher temperature performance cycles to improve fuel burn and emissions. This project is focused on the development of new high temperature turbine capability. The application of novel Ceramic Matrix Composites will be explored as a potential new material system in the core turbines. A number of other technologies including new alloy chemistry and protective coating developments will also be developed. Testing will be carried out at specimen, component and sub-system level in rigs and engines.
Category BEIS-Funded Programmes
Reference 113017
Status Closed
Funded period start 01/01/2014
Funded period end 31/03/2017
Funded value £6,302,733.00
Source https://gtr.ukri.org/projects?ref=113017

Participating Organisations

ROLLS-ROYCE PLC

£5,253,163.00

IMPERIAL COLLEGE OF SCIENCE, TECHNOLOGY AND MEDICINE

£120,000.00

SWANSEA UNIVERSITY

£929,570.00

The filing refers to a past date, and does not necessarily reflect the current state. The latest known state is available on the following page: Rolls-Royce plc, London.