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Engine representative internal cooling knowledge and applications

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€6 946 749
EU Contribution
€4 702 268
Project website
Project Acronym
ERICKA
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport sectors
Passenger transport

Overview

Call for proposal
FP7-AAT-2008-RTD-1
Link to CORDIS
Background & Policy context

Global air traffic is forecast to grow at an average annual rate of around 5% in the next 20 years. This high level of growth makes the need to address the environmental penalties of air traffic all the more urgent.

To reduce CO2 and NOX emissions new turbine cooling systems will be developed under the EU collaborative project ERICKA. The ERICKA project will aim at dramatically advancing greener Air Transport products that will:

  • reduce fuel consumption, CO2 and NOx emissions
  • encourage the rest of the aviation world to develop greener produce and reduce their ecological footprints
  • develop skills and knowledge throughout Europe.
Objectives

The objective of the ERICKA project is to directly contribute to the reduction in aircraft engine fuel consumption.

Developing new greener designs is essential to protect our environment. Thanks to an accelerated research process, ERICKA will contribute to a rapid progress in the introduction of green technologies into aviation. ERICKA will validate technology breakthroughs that are necessary to make major steps towards the environmental goals set by ACARE (Advisory Concil for Aeronautics Research in Europe) to be reached in 2020:

  • 50% reduction of CO2 emissions through drastic reduction of fuel consumption;
  • 80% reduction of NOx (nitrogen oxide) emission.
Methodology

The project, coordinated by Rolls-Royce, involves the main European aeronautic industrial organisations (Rolls-Royce, AVIO, MTU, Snecma) and other research institutes and universities from around Europe.

The members of ERICKA represent 18 organisations from 8 countries, among which: 7 industries,4 SME's, 3 Research Centres and 4 Universities.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
The European Commission
Type of funding
Public (EU)

Results

Improved cooling for future aero engines

Manufacturers of gas turbine engines are experimenting with continuously increasing operating temperatures to improve engine efficiency. EU-funded scientists developed technology and produced significant test results to find suitable cooling solutions.

Jet engine fuel efficiency largely depends on turbine performance. Turbine cooling system designs remain one of the most challenging parts of engine development, and designers rely heavily on empirical tools to produce new designs.

The EU-funded ERICKA (Engine representative internal cooling knowledge and applications) project conducted several tests in stationary and rotating test rigs to optimise cooling designs of turbine blades. Experimental work was supplemented by computational analysis and modelling.

Leading-edge cooling technology represents a critical area for improved gas turbine blade cooling design. A major part of the work was geared toward optimising the cooling performance of impingement systems. Different positions, angles and shapes for jet holes were tested to evaluate blade cooling performance. To achieve better results, the jet hole and fin positions were also shifted.

Project partners extensively investigated static and rotating cooling geometries typical of current and future engines. Experiments resulted in the selection of new geometries being designed, manufactured and tested.

ERICKA provided world-class measurement data of the heat transfer coefficient (HTC), and developed computational methods to advantageously exploit rotation to improve cooling design and turbine efficiency. Computational fluid dynamic analysis helped predict internal flows.

The project supported the development of design software specifically for designing cooling systems. Based on the HTC measurements, project partners developed code to find the optimum cooling passage designs for high- and low-pressure turbines. A database containing heat transfer data and pressure loss measurements from the optimised static rig geometry is available for download from the project website.

ERICKA aimed to reduce carbon dioxide emissions by 1 % compared to the year 2000 reference engines. The project significantly enhanced understanding of heat transfer and cooling to enable development of new cooling solutions. Project dissemination activities include a presentation and a poster presented at a workshop as well as the project website.

Partners

Lead Organisation
Organisation
Rolls Royce Plc
Address
65 Buckingham gate, LONDON, SW1E 6AT, United Kingdom
Organisation website
EU Contribution
€445 809
Partner Organisations
Organisation
Mtu Aero Engines
Address
Dachauer Strasse 665, 80995 MUENCHEN, Germany
Organisation website
EU Contribution
€233 000
Organisation
Safran Aircraft Engines
Address
2 Bvd Du General Martial-Valin, 75724 Paris, France
EU Contribution
€151 280
Organisation
Rolls-Royce Deutschland Ltd & Co Kg
Address
Eschenweg 11, 15827 BLANKENFELDE-MAHLOW, Germany
EU Contribution
€110 622
Organisation
General Electric (Switzerland) Gmbh
Address
Brown Boveri Strasse 7, 5401 Baden, Switzerland
EU Contribution
€202 500
Organisation
Universita Degli Studi Di Firenze
Address
Piazza San Marco 4, 50121 Florence, Italy
Organisation website
EU Contribution
€384 996
Organisation
Office National D'etudes Et De Recherches Aerospatiales
Address
CHEMIN DE LA HUNIERE, 91120 PALAISEAU, France
Organisation website
EU Contribution
€640 000
Organisation
Avio S.p.a.
Address
Via 1 Maggio 99, 00187 RIVALTA DI TORINO, Italy
Organisation website
EU Contribution
€0
Organisation
Instytut Maszyn Przeplywowych Im Roberta Szewalskiego Polskiej Akademii Nauk - Imp Pan
Address
Ul. Fiszera 14, 80N/A231 Gdansk, Poland
Organisation website
EU Contribution
€103 200
Organisation
Arttic
Address
58A rue du Dessous des Berges, 75013 PARIS, France
Organisation website
EU Contribution
€290 900
Organisation
Industria De Turbo Propulsores S.a.
Address
Parque Tecnológico, nº300, 48170 ZAMUDIO (VIZCAYA), Spain
Organisation website
EU Contribution
€200 850
Organisation
Enginsoft
Address
via della stazione 27, 38100 TRENTO, Italy
Organisation website
EU Contribution
€93 000
Organisation
Centre De Recherche En Aéronautique
Address
Batiment Eole, 1Er Étage - Rue Des Frères Wright 29, 6041 Gosselies, Belgium
Organisation website
EU Contribution
€240 955
Organisation
Ge Avio Srl
Address
VIA I MAGGIO 99, 10040 RIVALTA DI TORINO, Italy
Organisation website
EU Contribution
€87 459
Organisation
Numerical Mechanics Applications International Sa
Address
CHAUSSEE DE LA HULPE 187-189, 1170 BRUXELLES, Belgium
Organisation website
EU Contribution
€231 750
Organisation
Cambridge Flow Solutions Ltd
Address
163 Mill Road, Cambridge, CB1 3AN, United Kingdom
EU Contribution
€231 750
Organisation
The Chancellor Masters And Scholars Of The University Of Oxford
Address
University Offices, Wellington Square, OXFORD, OX1 2JD, United Kingdom
Organisation website
EU Contribution
€477 823
Organisation
Universitaet Paderborn
Address
Warburger Strasse 100, 33098 Paderborn, Germany
Organisation website
EU Contribution
€411 600
Organisation
Mtu Aero Engines
Address
Dachauer Strasse 665, 80995 MUENCHEN, Germany
Organisation website
EU Contribution
€0
Organisation
Universidad Politécnica De Madrid
Address
Avda. Ramiro de Maeztu, 3, 28040 MADRID, Spain
Organisation website
EU Contribution
€164 774

Technologies

Technology Theme
Aircraft propulsion
Technology
Highly efficient aircraft engine
Development phase
Validation

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