Coordinatore | ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
Organization address
address: Eschenweg 11 contact info |
Nazionalità Coordinatore | Germany [DE] |
Totale costo | 7˙411˙859 € |
EC contributo | 4˙899˙175 € |
Programma | FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics) |
Code Call | FP7-AAT-2010-RTD-1 |
Funding Scheme | CP-FP |
Anno di inizio | 2011 |
Periodo (anno-mese-giorno) | 2011-11-01 - 2016-05-31 |
# | ||||
---|---|---|---|---|
1 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
Organization address
address: Eschenweg 11 contact info |
DE (BLANKENFELDE-MAHLOW) | coordinator | 455˙596.95 |
2 |
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Organization address
address: Avenue de la Division Leclerc 29 contact info |
FR (CHATILLON) | participant | 800˙082.75 |
3 |
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
DE (KOELN) | participant | 599˙352.75 |
4 |
LOUGHBOROUGH UNIVERSITY
Organization address
address: Ashby Road contact info |
UK (LOUGHBOROUGH) | participant | 345˙750.00 |
5 |
UNIVERSITA DEGLI STUDI DI FIRENZE
Organization address
address: Piazza San Marco 4 contact info |
IT (Florence) | participant | 345˙000.00 |
6 |
GE AVIO SRL
Organization address
address: VIA I MAGGIO 99 contact info |
IT (RIVALTA DI TORINO) | participant | 264˙347.02 |
7 |
SNECMA SAS
Organization address
address: 2 Bvd du General Martial-Valin contact info |
FR (PARIS) | participant | 254˙917.50 |
8 |
UNIVERSITAET DER BUNDESWEHR MUENCHEN.
Organization address
address: WERNER HEISENBERG WEG 39 contact info |
DE (NEUBIBERG) | participant | 240˙000.00 |
9 |
INSTITUT NATIONAL DES SCIENCES APPLIQUEES DE ROUEN
Organization address
city: SAINT ETIENNE DU ROUVRAY contact info |
FR (SAINT ETIENNE DU ROUVRAY) | participant | 229˙321.20 |
10 |
TURBOMECA SA
Organization address
address: Avenue du President Szydlowski contact info |
FR (BORDES) | participant | 227˙544.50 |
11 |
ROLLS-ROYCE PLC
Organization address
address: BUCKINGHAM GATE 65 contact info |
UK (LONDON) | participant | 201˙000.00 |
12 |
Karlsruher Institut fuer Technologie
Organization address
address: Kaiserstrasse 12 contact info |
DE (Karlsruhe) | participant | 187˙560.00 |
13 |
THE CHANCELLOR, MASTERS AND SCHOLARS OF THE UNIVERSITY OF CAMBRIDGE
Organization address
address: The Old Schools, Trinity Lane contact info |
UK (CAMBRIDGE) | participant | 184˙536.00 |
14 |
ARTTIC
Organization address
address: Rue du Dessous des Berges 58A contact info |
FR (PARIS) | participant | 146˙888.00 |
15 |
IMPERIAL COLLEGE OF SCIENCE, TECHNOLOGY AND MEDICINE
Organization address
address: SOUTH KENSINGTON CAMPUS EXHIBITION ROAD contact info |
UK (LONDON) | participant | 96˙735.60 |
16 |
UNIVERSITE DE PAU ET DES PAYS DE L'ADOUR
Organization address
address: Avenue de l'Universite contact info |
FR (PAU) | participant | 93˙000.00 |
17 |
AVIO S.P.A
Organization address
address: Strada del Drosso 145 contact info |
IT (TORINO) | participant | 82˙402.98 |
18 |
Cambridge Flow Solutions Ltd
Organization address
address: 163 Mill Road contact info |
UK (Cambridge) | participant | 76˙239.75 |
19 |
MTU AERO ENGINES AG
Organization address
address: DACHAUER STRASSE 665 contact info |
DE (MUNCHEN) | participant | 68˙900.00 |
20 |
AVIOPROP SRL
Organization address
address: VIA PAPA GIOVANNI XXIII 9 contact info |
IT (CAMERI) | participant | 0.00 |
21 |
MTU AERO ENGINES GMBH
Organization address
address: "Dachauer Strasse, 665" contact info |
DE (MUENCHEN) | participant | 0.00 |
Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.
'The environmental benefits of low emissions lean burn technology in reducing NOx emissions up to 80% will only be effective when these are deployed to a large range of new aero-engine applications. While integrating and developing low emission combustion design rules, IMPACT-AE will deliver novel combustor design methodologies for advanced engine architectures and thermodynamic cycles. It will support European engine manufacturers to pick up and keep pace with the US competitors, being already able to exploit their new low emission combustion technology to various engine applications with short turn-around times. Key element of the project will be the development and validation of design methods for low emissions combustors to reduce NOx and CO emissions by an optimization of the combustor aero-design process. Preliminary combustor design tools will be coupled with advanced parametrisation and automation tools. Improved heat transfer and NOx models will increase the accuracy of the numerical prediction. The advanced representation of low emission combustors and the capability to investigate combustor scaling effects allow an efficient optimisation of future combustors targeting a cut of combustor development time by 50%. IMPACT-AE is split into four technical work packages: WP1‘Development of smart design methodologies for clean combustion’ as central WP to deliver the new methodology for combustor design, WP2’Modelling and design of advanced combustor wall cooling concepts’ for combustor liner design definition as key technology area, WP3’Technology validation by detailed flame diagnostics’ to substantiate fuel injector design rules implemented into the design methodology and WP4’Methodology demonstration for efficient low NOx combustors’ will validate the combustor design. The consortium consists of all major aero-engine manufactures in Europe, 7 universities and 3 research establishments with recognised experience in low emission combustion research and 10 SMEs.'
An EU-funded initiative is improving the design process for low-emission combustors for aero-engines, which will dramatically reduce development time.
The 'Intelligent design methodologies for low pollutant combustors for aero-engines' (http://www.impact-ae.eu/ (IMPACT-AE)) project will develop and validate smart design systems for highly efficient aero-engine combustors centred on lean burn engines. This is based on the concept that excess air introduced into the engine will lower the temperature of the combustion process. This in turn will reduce the amount of nitrogen oxides (NOx) produced.
IMPACT-AE brings together all the major aero-engine manufacturers in Europe with universities, research establishments and small and medium-sized enterprises. The aim is to develop new methods for designing improved combustors capable of reducing NOx and carbon monoxide (CO) emissions.
Project partners are developing new design tools and improving models of heat transfer and NOx. The advanced representation of low-emission combustors and the ability to investigate scaling effects will help reduce combustor development time by half. Research is focused on the new methodology for combustor design and the modelling of advanced combustor wall cooling concepts.
Key elements for low-emissions combustor design systems were developed, combustor models created, and the generation of meshes for computational fluid dynamic calculations were automated. The design process is also being automated and linked to preliminary design methods.
Simultaneously, the consortium is carrying out an assessment of rapid manufacturing technologies for combustor components like fuel injectors. Flame diagnostics are currently being performed to assess the new combustion technology and test rigs were established to validate the low-emission combustor design methodology.
IMPACT-AE will significantly reduce the time required for developing combustors compared to other state-of-the-art processes. It will also help reduce CO and NOx emissions and provide a blue print for future aero-engine design. Successful outcomes will help reduce pollution while enabling European manufacturers to compete more effectively with global competitors.