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Financement britannique (5 029 492 £) : Projet SILOET 6 - Validation de la technologie de base : Systèmes Ukri 01/05/2009 Recherche et innovation du Royaume-Uni, Royaume Uni
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Projet SILOET 6 - Validation de la technologie de base : Systèmes
| Abstract | Work done to date on aerospace gas turbine lean burn combustion systems, and turbine tip clearance control systems, on the ANTLE and EFE demonstrator programmes has identified that there are significant challenges beyond the “conventional” scope of combustor and turbine tip clearance technologies. For example, the lean burn combustion system needs to be able to address the, sometimes conflicting, requirements of providing fuel to separate pilot and mains feeds within the burner, but without introducing regions of stagnant hot fuel with the associated risk of coking, and without complex pipe arrangements that would influence the response time of the system to demanded power change. It is essential that capability is developed in the related systems that control their operation and that these systems are fully integrated into the whole engine architecture. The objectives of this project are to increase the Technology Readiness Level of the full system capability needed to complement a lean burn combustor, and to deliver improved tip clearance control capability beyond that planned in existing programmes. |
| Category | BEIS-Funded Programmes |
| Reference | 110035 |
| Status | Closed |
| Funded period start | 01/05/2009 |
| Funded period end | 30/04/2013 |
| Funded value | £5 029 492,00 |
| Source | https://gtr.ukri.org/projects?ref=110035 |
Participating Organisations
| ROLLS-ROYCE PLC |
£4 773 464,00 |
| UNIVERSITY OF OXFORD |
£134 910,00 |
| LOUGHBOROUGH COLLEGE LOUGHBOROUGH |
£121 118,00 |
Cette annonce se réfère à une date antérieure et ne reflète pas nécessairement l’état actuel. L’état actuel est présenté à la page suivante : Rolls-Royce plc, Londres, Royaume Uni.
