DYNAMO

DYNAMO Design methods for durabilitY aNd operAbility of low eMissions cOmbustors

 Coordinatore LOUGHBOROUGH UNIVERSITY 

 Organization address address: Ashby Road
city: LOUGHBOROUGH
postcode: LE11 3TU

contact info
Titolo: Dr.
Nome: Christopher
Cognome: Malins
Email: send email
Telefono: +44 1509 222421

 Nazionalità Coordinatore United Kingdom [UK]
 Totale costo 796˙529 €
 EC contributo 597˙395 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2013-01
 Funding Scheme JTI-CS
 Anno di inizio 2014
 Periodo (anno-mese-giorno) 2014-01-01   -   2016-12-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    LOUGHBOROUGH UNIVERSITY

 Organization address address: Ashby Road
city: LOUGHBOROUGH
postcode: LE11 3TU

contact info
Titolo: Dr.
Nome: Christopher
Cognome: Malins
Email: send email
Telefono: +44 1509 222421

UK (LOUGHBOROUGH) coordinator 312˙298.00
2    UNIVERSITY OF SOUTHAMPTON

 Organization address address: Highfield
city: SOUTHAMPTON
postcode: SO17 1BJ

contact info
Titolo: Mrs.
Nome: Yan
Cognome: Qiao
Email: send email
Telefono: +44 2380593907

UK (SOUTHAMPTON) participant 149˙762.00
3    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: +44 1223333534

UK (CAMBRIDGE) participant 135˙335.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

acoustics    thermo    temperature    combustion    lean    burn    loughborough    university    instabilities    data    emissions    durability    combustor    transfer    fuel    radiative    resolve    heat    software    models    validated    experimental   

 Obiettivo del progetto (Objective)

'Design methods for durabilitY aNd operAbility of low eMissions cOmbustors: DYNAMO

Lean burn combustor systems are a key technology to reduce NOx emissions for future engines. The ability to maintain the desired combustor metal temperature is critical to achieving acceptable durability. The levels of fuel-air premixing inherent in lean burn designs makes them susceptible to thermo-acoustics instabilities which will have a drastic impact on the durability of the combustor. The overall aim of this project is to develop validated methodologies for the prediction of combustor temperature and thermo-acoustics instabilities to allow confident design of the combustion system of a demonstrator engine at TRL6. The first work package focusses on cooling and radiative heat transfer. It uses Computational Fluid Dynamics to highly resolve the combustor liner geometric features so that a cheaper model may be obtained for design purposes. In addition the sensitivity of radiative heat transfer to the choice of physics models is assessed. The resulting models will be validated against existing experimental data from Loughborough University and the industrial partner. The second work package develops a smart system for combustor design by bringing together a variety of analysis techniques and creating software that can directly drive CAD software. A response surface supported by multi-fidelity, multi-objective robust design approaches will be used to deliver a world class combustor design process. Thermoacoustics are considered by using CFD to study the response of a fuel injector to acoustic plane waves and by modelling a complete annular combustion system in order to resolve circumferential modes. The thermoacoustic results will be validated against existing experimental data available at Loughborough and Cambridge University.'

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