FACTOR
Full Aero-thermal Combustor-Turbine interactiOn Research
| Coordinatore | SNECMA SAS
Organization address
address: 2 Bvd du General Martial-Valin contact info |
| Nazionalità Coordinatore | France [FR] |
| Totale costo | 7˙235˙256 € |
| EC contributo | 4˙893˙945 € |
| Programma | FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics) |
| Code Call | FP7-AAT-2010-RTD-1 |
| Funding Scheme | CP-FP |
| Anno di inizio | 2010 |
| Periodo (anno-mese-giorno) | 2010-12-01 - 2016-11-30 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
SNECMA SAS
Organization address
address: 2 Bvd du General Martial-Valin contact info |
FR (PARIS) | coordinator | 275˙301.00 |
| 2 |
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
DE (KOELN) | participant | 1˙403˙170.24 |
| 3 |
PROGESA S.R.L.
Organization address
address: VIA ROMOLO GESSI 37 contact info |
IT (BRESCIA) | participant | 367˙392.00 |
| 4 |
THE CHANCELLOR, MASTERS AND SCHOLARS OF THE UNIVERSITY OF OXFORD
Organization address
address: University Offices, Wellington Square contact info |
UK (OXFORD) | participant | 292˙187.70 |
| 5 |
THE CHANCELLOR, MASTERS AND SCHOLARS OF THE UNIVERSITY OF CAMBRIDGE
Organization address
address: The Old Schools, Trinity Lane contact info |
UK (CAMBRIDGE) | participant | 257˙264.00 |
| 6 |
INSTITUT VON KARMAN DE DYNAMIQUE DES FLUIDES
Organization address
address: CHAUSSEE DE WATERLOO 72 contact info |
BE (RHODE SAINT GENESE) | participant | 257˙246.00 |
| 7 |
ARTTIC
Organization address
address: Rue du Dessous des Berges 58A contact info |
FR (PARIS) | participant | 230˙296.00 |
| 8 |
UNIVERSITA DEGLI STUDI DI FIRENZE
Organization address
address: Piazza San Marco 4 contact info |
IT (Florence) | participant | 204˙697.00 |
| 9 |
INSTYTUT MASZYN PRZEPLYWOWYCH IM ROBERTA SZEWALSKIEGO POLSKIEJ AKADEMII NAUK - IMP PAN
Organization address
address: UL. FISZERA 14 contact info |
PL (GDANSK) | participant | 155˙235.70 |
| 10 |
TURBOMECA SA
Organization address
address: Avenue du President Szydlowski contact info |
FR (BORDES) | participant | 153˙414.00 |
| 11 |
CENTRE EUROPEEN DE RECHERCHE ET DE FORMATION AVANCEE EN CALCUL SCIENTIFIQUE
Organization address
address: Avenue Gaspard Coriolis 42 contact info |
FR (TOULOUSE) | participant | 148˙468.00 |
| 12 |
ROLLS-ROYCE PLC
Organization address
address: BUCKINGHAM GATE 65 contact info |
UK (LONDON) | participant | 147˙588.00 |
| 13 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
Organization address
address: Eschenweg 11 contact info |
DE (BLANKENFELDE-MAHLOW) | participant | 138˙151.00 |
| 14 |
GLOBAL DESIGN TECHNOLOGY SA
Organization address
city: LIEGE (Angleur) contact info |
BE (LIEGE (Angleur)) | participant | 110˙737.00 |
| 15 |
SIEMENS INDUSTRIAL TURBOMACHINERY AB
Organization address
address: - contact info |
SE (FINSPONG) | participant | 97˙020.00 |
| 16 |
MTU AERO ENGINES AG
Organization address
address: DACHAUER STRASSE 665 contact info |
DE (MUNCHEN) | participant | 96˙118.00 |
| 17 |
ILA INTELLIGENT LASER APPLICATIONS GMBH
Organization address
address: Karl-Heinz-Beckurts Strasse 13 contact info |
DE (JULICH) | participant | 95˙548.00 |
| 18 |
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Organization address
address: Avenue de la Division Leclerc 29 contact info |
FR (CHATILLON) | participant | 95˙546.00 |
| 19 |
INDUSTRIA DE TURBO PROPULSORES S.A.
Organization address
address: PARQUE TECNOLOGICO DE ZAMUDIO 300 contact info |
ES (ZAMUDIO-VIZCAYA) | participant | 95˙394.00 |
| 20 |
GKN AEROSPACE SWEDEN AB
Organization address
address: - contact info |
SE (TROLLHAETTAN) | participant | 89˙880.99 |
| 21 |
PRATT & WHITNEY RZESZOW SPOLKA AKCYJNA
Organization address
address: ULICA HETMANSKA 120 contact info |
PL (RZESZOW) | participant | 71˙925.50 |
| 22 |
GE AVIO SRL
Organization address
address: VIA I MAGGIO 99 contact info |
IT (RIVALTA DI TORINO) | participant | 56˙108.12 |
| 23 |
AVIO S.P.A
Organization address
address: Strada del Drosso 145 contact info |
IT (TORINO) | participant | 55˙256.75 |
| 24 |
MTU AERO ENGINES GMBH
Organization address
address: "Dachauer Strasse, 665" contact info |
DE (MUENCHEN) | participant | 0.00 |
Mappa
Word cloud
Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.
Obiettivo del progetto (Objective)
'To achieve lower Specific Fuel Consumption (SFC) and CO2/NOx emissions, modern turbomachineries operate at high velocities and high temperature conditions. The lack of confidence in the prediction of combustor-turbine interactions leads to apply extra safety margins on components design. Therefore, the understanding of combustor-turbine flow field interactions is mandatory to preserve High Pressure Turbine (HPT) life and performance when optimising the design of new HPT. The FACTOR objective is to optimise the combustor turbine interactions design to develop low-cost turbines and reduce SFC by 2%, HPT weight by 1.5% and accordingly engine cost by 3% compared to the results from the TATEF2 and AITEB2 projects. To achieve this objective, FACTOR will develop and exploit an innovative test infrastructure coupling a combustor simulator with a HPT for aerodynamic and aerothermal measurements. The infrastructure will improve the knowledge of aerothermal external flows since the inlet profile of the turbine and the secondary flows will be modelled and optimised together in the same facility, under engine representative conditions. Collected data will be fed into the design techniques and simulation software used to optimise HPT components. In parallel, the use of advanced CFD (e.g. LES or DES) will provide new knowledge on wall temperature and heat transfer predictions. This will be particularly important to design future combustor-turbine systems in an integrated manner, especially for the next generation of lean burn combustion systems having complex and severe flow constraints. By optimising the combustor-HPT interaction, FACTOR project will contribute to achieving the 50% CO2 and 80% NOx reductions ACARE 2020 environmental objectives. FACTOR will also strengthen the competitiveness of the European aeroengine industry by making available a new test infrastructure with experimental abilities beyond those of the US.'
Introduzione (Teaser)
Gas turbine performance strongly depends on the flow field inside the combustor. EU-funded scientists advanced aero engine design by treating the combustor and turbine as a system instead of optimising each component separately.