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Research on Core Noise Reduction

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€5 935 211
EU Contribution
€4 008 962
Project Acronym
RECORD
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Decarbonisation,
Environmental/Emissions aspects
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
FP7-AAT-2012-RTD-1
Link to CORDIS
Background & Policy context

In order to achieve the greening of the European air transport with the deployment of low emission and low noise propulsion systems the reduction of core noise plays an important role. The ability to design low core noise aero-engines requires the development of reliable prediction tools. This development demands extensive research with dedicated experimental test cases and sophisticated numerical and analytical modelling work to broaden the physical understanding of core noise generation mechanisms.

Objectives

This objective is only reachable with an extensive cooperation on the European level. In the Research on Core Noise Reduction (RECORD) project the major aero-engine manufacturers of five different European countries collaborate in order to enable the design of low core noise aero-engines.

Methodology

In RECORD the fundamental understanding of core noise generation and how can it be reduced will be achieved by combining the research competence of all European experts in universities and research organizations working in this field of core noise. This concept of the RECORD project is completed by the technology development of small and medium size enterprises distributed in Europe.

RECORD will promote the understanding of noise generating mechanism and its propagation taking the interaction of combustor and turbine into account. The importance of direct and indirect noise will be quantified. Through carefully designed experiments and extensive numerical calculations, the numerical methods and assumptions will be validated and extended. As a result, low-order models will provide a quick approach for the noise design of combustors and subsequent turbine stages while the more time-consuming and expensive LES calculation will provide a more detailed picture of the flow physics. Finally, RECORD will develop means and methods for core noise reduction.

Funding

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

Results

Quieter aircraft core engines

EU-funded researchers are devoting extensive research to improve understanding and reducing of combustion noise and its sources in aircraft engines.

Reduction of aero engine emissions and noise plays an important role in Europe's target for a greener air transport system. Combustion noise is a potential major contributor to the overall noise emitted by low-emission engines. This accounts for the increased interest in development of reliable noise prediction tools for modern aero engines.

The EU-funded project 'Research on core noise reduction' (RECORD) is enhancing understanding of core noise-generating mechanisms and its propagation, also taking combustor-turbine interaction into account. An important focus will be on the direct and indirect combustion noise mechanisms.

RECORD is using diverse prediction methods for core noise, ranging from low-order modelling approaches to high-fidelity compressible large eddy simulations. The former will help with low-noise designs of combustors and subsequent turbine stages, while the latter will provide a more detailed picture of flow fields.

Through carefully designed experiments and extensive numerical calculations, these methods will be validated and extended.

Scientists have drafted all relevant specifications with the aim of defining three test cases: The prediction methods for entropy and vorticity noises in transonic nozzles are currently being validated using the Nozzle Test Case.

Within the Combustor Test Case the combustion chamber has been modified with a thermally stabilised, water-cooled casing. The experimental tests of this new set-up are ongoing. Scientists made good progress concerning the numerical simulations.

Extensive test rig modifications in the Turbine Test Case have been achieved to enable a detailed analysis of sound transmission through a turbine stage and sound generation by inflow disturbances. A numerical benchmark test of the undisturbed turbine flow test has allowed comparison of the different applied numerical methods.

Through better understanding of this complex noise sources, RECORD should be able to provide designs for reduced noise of relevant components such as combustors and turbines.

RECORD should also provide tools that will allow trade-offs between noise and emissions and allow the development of low-noise technologies. Its objectives are in line with the Advisory Council for Aeronautics Research in Europe's (ACARE) Vision 2020 for reducing the perceived noise by 50 %.

Partners

Lead Organisation
Organisation
Deutsches Zentrum Fr Luft Und Raumfahrt E.v
Address
Linder Hoehe, 51147 KOELN, Germany
Organisation website
EU Contribution
€790 756
Partner Organisations
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
€300 000
Organisation
Safran Aircraft Engines
Address
2 Bvd Du General Martial-Valin, 75724 Paris, France
EU Contribution
€85 150
Organisation
Sandu M. Constantin Persoana Fizica
Address
Ripiceni, Bl.5, Apt.40, Sect.2, 23624 Bucharest, Romania
Organisation website
EU Contribution
€75 000
Organisation
Rolls-Royce Deutschland Ltd & Co Kg
Address
Eschenweg 11, 15827 BLANKENFELDE-MAHLOW, Germany
EU Contribution
€70 000
Organisation
Technische Universitaet Muenchen
Address
Arcisstrasse 21, 80333 MUENCHEN, Germany
Organisation website
EU Contribution
€266 880
Organisation
Universita Degli Studi Di Firenze
Address
Piazza San Marco 4, 50121 Florence, Italy
Organisation website
EU Contribution
€150 664
Organisation
Safran Helicopter Engines
Address
Avenue Du President Szydlowski, 64510 Bordes, France
EU Contribution
€209 742
Organisation
Office National D'etudes Et De Recherches Aerospatiales
Address
CHEMIN DE LA HUNIERE, 91120 PALAISEAU, France
Organisation website
EU Contribution
€150 780
Organisation
Msc Software Belgium
Address
Rue Emile Francqui 1 Axis Park, 1435 Mont Saint Guibert, Belgium
Organisation website
EU Contribution
€77 000
Organisation
Centre Europeen De Recherche Et De Formation Avancee En Calcul Scientifique
Address
Avenue Gaspard Coriolis 42, 31057 Toulouse, France
Organisation website
EU Contribution
€336 710
Organisation
Avio S.p.a.
Address
Via 1 Maggio 99, 00187 RIVALTA DI TORINO, Italy
Organisation website
EU Contribution
€0
Organisation
Industria De Turbo Propulsores S.a.
Address
Parque Tecnológico, nº300, 48170 ZAMUDIO (VIZCAYA), Spain
Organisation website
EU Contribution
€67 083
Organisation
Politecnico Di Milano
Address
Piazza Leonardo Da Vinci 32, 20133 Milano, Italy
Organisation website
EU Contribution
€303 778
Organisation
Ge Avio Srl
Address
VIA I MAGGIO 99, 10040 RIVALTA DI TORINO, Italy
Organisation website
EU Contribution
€78 000
Organisation
Technische Universitat Darmstadt
Address
KAROLINENPLATZ 5, 64289 DARMSTADT, Germany
Organisation website
EU Contribution
€226 200
Organisation
Cave S.r.l
Address
Via Domenichino 19, 20149 Milano, Italy
EU Contribution
€90 000
Organisation
Rolls Royce Plc
Address
65 Buckingham gate, LONDON, SW1E 6AT, United Kingdom
Organisation website
EU Contribution
€180 190
Organisation
Centre National De La Recherche Scientifique
Address
3 rue Michel-Ange, 75794 PARIS, France
Organisation website
EU Contribution
€401 320
Organisation
Universidad Politécnica De Madrid
Address
Avda. Ramiro de Maeztu, 3, 28040 MADRID, Spain
Organisation website
EU Contribution
€149 709

Technologies

Technology Theme
Noise testing, modelling and reduction
Technology
Engine core noise measurements
Development phase
Research/Invention

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