Explore the words cloud of the TurboNoiseBB project. It provides you a very rough idea of what is the project "TurboNoiseBB" about.
The following table provides information about the project.
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
|Coordinator Country||Germany [DE]|
|Total cost||6˙702˙851 €|
|EC max contribution||6˙702˙851 € (100%)|
1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
|Duration (year-month-day)||from 2016-09-01 to 2020-02-29|
Take a look of project's partnership.
|1||DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV||DE (KOELN)||coordinator||898˙647.00|
|2||ROLLS-ROYCE PLC||UK (LONDON)||participant||955˙250.00|
|3||AIRBUS OPERATIONS SAS||FR (TOULOUSE)||participant||621˙427.00|
|4||SAFRAN AIRCRAFT ENGINES||FR (PARIS)||participant||611˙937.00|
|5||UNIVERSITY OF SOUTHAMPTON||UK (SOUTHAMPTON)||participant||608˙367.00|
|6||GKN AEROSPACE SWEDEN AB||SE (TROLLHAETTAN)||participant||582˙400.00|
|7||OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES||FR (PALAISEAU)||participant||501˙075.00|
|8||CHALMERS TEKNISKA HOEGSKOLA AB||SE (GOETEBORG)||participant||320˙632.00|
|9||MTU AERO ENGINES AG||DE (MUNCHEN)||participant||301˙700.00|
|10||ECOLE CENTRALE DE LYON||FR (ECULLY)||participant||300˙000.00|
|11||INDUSTRIA DE TURBO PROPULSORES S.A.U.||ES (ZAMUDIO-VIZCAYA)||participant||282˙000.00|
|12||SAFRAN HELICOPTER ENGINES||FR (BORDES)||participant||250˙003.00|
|13||UNIVERSIDAD POLITECNICA DE MADRID||ES (MADRID)||participant||200˙000.00|
|14||THE CHANCELLOR MASTERS AND SCHOLARSOF THE UNIVERSITY OF CAMBRIDGE||UK (CAMBRIDGE)||participant||170˙000.00|
|15||STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM||NL (AMSTERDAM)||participant||99˙410.00|
TurboNoiseBB aims to deliver reliable prediction methodologies and noise reduction technologies in order to allow European Aerospace industries: • to design low-noise aircraft to meet society’s needs for more environmentally friendly air transport • to win global leadership for European aeronautics with a competitive supply chain. The project is focusing on fan broadband (BB) noise sources and will offer the possibility to acquire an experimental database mandatory to validate the Computational Fluid Dynamics and Aero Acoustic (CAA) simulations from the sound sources to the radiation from aircraft engines. It fully exploits the methodology successfully developed starting from FP5 programmes, TurboNoiseCFD and AROMA and also associated FP6 (SILENCE(R), PROBAND, OPENAIR) and FP7 (FLOCON, TEENI, ENOVAL) proposals.
TurboNoiseBB has 3 main objectives. 1. To acquire appropriate CAA validation data on a representative test model. In addition different approaches for measuring the BB far-field noise levels in the rear arc (bypass duct contribution) will be assessed to help define future requirements for European turbofan test facilities. 2. To apply and validate CAA codes with respect to fan & turbine BB noise. 3. To design novel low BB noise fan systems by means of state-of-the-art design and prediction tools.
The combination of partners from industry, research university combined with the excellence of the EU most versatile test facility for aero and noise forms the basis for the successful validation and exploitation of CAA methods, crucial for quicker implementation of future low noise engine concepts. TurboNoiseBB will deliver validated industry-exploitable aeroacoustic design prediction tools related to BB noise emissions from aircraft nacelle intakes exhaust nozzles, allowing EU industry to leap-frog NASA-funded technology developments in the US. It will also deliver a technical assessment on the way forward for European turbofan noise testing.
|TurboNoiseBB internet presence (website)||Websites, patent fillings, videos etc.||2020-01-22 10:02:25|
Take a look to the deliverables list in detail: detailed list of TurboNoiseBB deliverables.
|year||authors and title||journal||last update|
Robert K.J. Meyer - German Aerospace Center (DLR)
Sebastian Hakansson - German Aerospace Center (DLR)
Wolfram Hage - German Aerospace Center (DLR)
Lars Enghardt - German Aerospace Center (DLR)
Instantaneous flow field measurements in the interstage section between a fan and the outlet guiding vanes at different axial positions
published pages: , ISSN: , DOI:
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The information about "TURBONOISEBB" are provided by the European Opendata Portal: CORDIS opendata.