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Intelligent Design Methodologies for Low Pollutant Combustors for Aero-Engines

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€7 411 860
EU Contribution
€4 899 175
Project website
Project Acronym
IMPACT-AE
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Decarbonisation
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
FP7-AAT-2010-RTD-1
Link to CORDIS
Background & Policy context

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 combustion chamber design methodologies for advanced engine architectures and thermodynamic cycles.

Objectives

The IMPACT-AE project will support European engine manufacturers to pick up and keep pace with 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 combustion chambers to reduce NOx and CO emissions by optimisation of the combustion chamber aero-design process.

Methodology

Preliminary combustion chamber design tools will be coupled with advanced parameterisation and automation tools. Improved heat transfer and NOx models will increase the accuracy of the numerical prediction. The advanced representation of low emission combustion chambers and the capability to investigate combustion chamber scaling effects, allow an efficient optimisation of future combustion chambers targeting a cut of combustion chamber development time by 50%.

IMPACT-AE is split into four technical work packages:

  • WP1Development of smart design methodologies for clean combustion as central WP to deliver the new methodology for combustion chamber design;
  • WP2Modelling and design of advanced combustion chamber wall cooling concepts for combustion chamber liner design definition as key technology area;
  • WP3Technology validation by detailed flame diagnostics to substantiate fuel injector design rules implemented into the design methodology;
  • WP4Methodology demonstration for efficient low NOx combustion chambers will validate the combustion chamber 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.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
The European Commission
Type of funding
Public (EU)
Specific funding programme
FP7-TRANSPORT

Results

Improving design for cleaner aero-engines

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.

Partners

Lead Organisation
Organisation
Rolls-Royce Deutschland Ltd & Co Kg
Address
Eschenweg 11, 15827 BLANKENFELDE-MAHLOW, Germany
EU Contribution
€455 597
Partner Organisations
Organisation
Institut National Des Sciences Appliquees De Rouen
Address
Avenue de l'Université, 76 801 SAINT ETIENNE DU ROUVRAY, France
Organisation website
EU Contribution
€229 321
Organisation
The Chancellor Masters And Scholars Of The University Of Cambridge
Address
TRINITY LANE THE OLD SCHOOLS, CAMBRIDGE, CB2 1TN, United Kingdom
Organisation website
EU Contribution
€184 536
Organisation
Mtu Aero Engines
Address
Dachauer Strasse 665, 80995 MUENCHEN, Germany
Organisation website
EU Contribution
€0
Organisation
Imperial College Of Science Technology And Medicine
Address
Exhibition Road, South Kensington, LONDON, SW7 2AZ, United Kingdom
Organisation website
EU Contribution
€96 736
Organisation
Safran Aircraft Engines
Address
2 Bvd Du General Martial-Valin, 75724 Paris, France
EU Contribution
€254 918
Organisation
Universite De Pau Et Des Pays De L'adour
Address
Avenue De L'universite, 64000 Pau, France
EU Contribution
€93 000
Organisation
Universita Degli Studi Di Firenze
Address
Piazza San Marco 4, 50121 Florence, Italy
Organisation website
EU Contribution
€345 000
Organisation
Avioprop Srl
Address
VIA PAPA GIOVANNI XXIII 9, 28062 CAMERI, Italy
Organisation website
EU Contribution
€0
Organisation
Safran Helicopter Engines
Address
Avenue Du President Szydlowski, 64510 Bordes, France
EU Contribution
€227 545
Organisation
Office National D' Etudes Et De Recherches Aérospatiales
Address
29, avenue de la Division Leclerc, BP72 CHÂTILLON CEDEX, France
Organisation website
EU Contribution
€800 083
Organisation
Deutsches Zentrum Fr Luft Und Raumfahrt E.v
Address
Linder Hoehe, 51147 KOELN, Germany
Organisation website
EU Contribution
€599 353
Organisation
Avio S.p.a.
Address
Via 1 Maggio 99, 00187 RIVALTA DI TORINO, Italy
Organisation website
EU Contribution
€82 403
Organisation
Karlsruher Institut Fuer Technologie
Address
Kaiserstrasse, 76131 Karlsruhe, Germany
Organisation website
EU Contribution
€187 560
Organisation
Arttic
Address
58A rue du Dessous des Berges, 75013 PARIS, France
Organisation website
EU Contribution
€146 888
Organisation
Loughborough University
Address
Ashby Road, Loughborough, LE11 3TU, United Kingdom
Organisation website
EU Contribution
€345 750
Organisation
Ge Avio Srl
Address
Via Papa Giovanni Xxiii 9, 28062 Cameri, Italy
EU Contribution
€264 347
Organisation
Cambridge Flow Solutions Ltd
Address
163 Mill Road, Cambridge, CB1 3AN, United Kingdom
EU Contribution
€76 240
Organisation
Rolls Royce Plc
Address
65 Buckingham gate, LONDON, SW1E 6AT, United Kingdom
Organisation website
EU Contribution
€201 000
Organisation
Universitaet Der Bundeswehr Muenchen
Address
Werner Heisenberg Weg 39, 85577 Neubiberg, Germany
Organisation website
EU Contribution
€240 000
Organisation
Mtu Aero Engines
Address
Dachauer Strasse 665, 80995 MUENCHEN, Germany
Organisation website
EU Contribution
€68 900

Technologies

Technology Theme
Aircraft propulsion
Technology
Combustor design for low emissions and/or high turbine efficiency
Development phase
Research/Invention

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