AMEL

Advanced Methods for the Prediction of Lean-burn Combustor Unsteady Phenomena

Coordinatore	THE CHANCELLOR, MASTERS AND SCHOLARS OF THE UNIVERSITY OF CAMBRIDGE    more  Organization address address: The Old Schools, Trinity Lane city: CAMBRIDGE postcode: CB2 1TN contact info Titolo: Ms. Nome: Renata Cognome: Schaeffer Email: send email Telefono: 441223000000 Fax: +441223 332988
Nazionalità Coordinatore	United Kingdom [UK]
Totale costo	815˙359 €
EC contributo	611˙519 €
Programma	FP7-JTI Specific Programme "Cooperation": Joint Technology Initiatives
Code Call	SP1-JTI-CS-2013-03
Funding Scheme	JTI-CS
Anno di inizio	2014
Periodo (anno-mese-giorno)	2014-12-01   -   2016-05-31

 Partecipanti

#	participant	country	role	EC contrib. [€]
1	THE CHANCELLOR, MASTERS AND SCHOLARS OF THE UNIVERSITY OF CAMBRIDGE  Organization address address: The Old Schools, Trinity Lane city: CAMBRIDGE postcode: CB2 1TN contact info Titolo: Ms. Nome: Renata Cognome: Schaeffer Email: send email Telefono: 441223000000 Fax: +441223 332988	UK (CAMBRIDGE)	coordinator	487˙774.66
2	LOUGHBOROUGH UNIVERSITY  Organization address address: Ashby Road city: LOUGHBOROUGH postcode: LE11 3TU contact info Titolo: Dr. Nome: Christopher Cognome: Malins Email: send email Telefono: 441509000000	UK (LOUGHBOROUGH)	participant	123˙745.20

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 Obiettivo del progetto (Objective)

'The development of lean-burn gas turbine combustors, which will lead to a reduction of emissions from aviation, relies upon resolving significant problems associated with this new technology, namely the emergence of combustion-induced pressure oscillations that can damage the engine, and the danger of flame extinction, which may not allow the full benefits of lean-burn to be realised. Apart from their very significant practical importance, these phenomena are very challenging scientifically and a complete theoretical treatment is not available at present.

In this proposal, simulation tools for advanced cooling methods, for thermoacoustics, and for flame extinction will be developed, enabled by recent theoretical, computational, and experimental developments. These tools will be based on low-order models and more complex Computational Fluid Dynamics methods, both validated against focused experiments in single-sector, multi-sector, and full annular geometries. The results will assist engine manufacturers assess ideas and designs at low TRL levels, which will decrease the development time and the high cost associated with testing at high TRL.'