ALIAS

Acoustic Liners for air conditioning system

 Coordinatore OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES 

 Organization address address: Avenue de la Division Leclerc 29
city: CHATILLON
postcode: 92322

contact info
Nome: Luc
Cognome: Bignon
Email: send email
Telefono: +33 5 62252581
Fax: +33 5 62252583

 Nazionalità Coordinatore France [FR]
 Totale costo 299˙976 €
 EC contributo 179˙405 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2012-02
 Funding Scheme JTI-CS
 Anno di inizio 2013
 Periodo (anno-mese-giorno) 2013-01-01   -   2015-05-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES

 Organization address address: Avenue de la Division Leclerc 29
city: CHATILLON
postcode: 92322

contact info
Nome: Luc
Cognome: Bignon
Email: send email
Telefono: +33 5 62252581
Fax: +33 5 62252583

FR (CHATILLON) coordinator 91˙154.00
2    ATECA SAS

 Organization address address: LIEU DIT VERLHAGUET
city: MONTAUBAN
postcode: 82000

contact info
Titolo: Mrs.
Nome: Valia
Cognome: Fascio
Email: send email
Telefono: +33 563637897

FR (MONTAUBAN) participant 88˙251.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

impedance    treatments    configuration    flow    conditioning    liners    reacting    attenuation    procedure    locally    cfp    industrial    manufactured    solution    code    air    acoustic    then    noise    frequency   

 Obiettivo del progetto (Objective)

'The ALIAS project consists in designing optimized locally reacting treatments for mid-frequency acoustic attenuation in air conditioning system. The French Aerospace Lab (ONERA) and the SME ATECA, specialized in Aeronautics, Advanced Materials & Manufacturing, will combine their research and technological capabilities to propose a solution of TRL5 that meets the industrial requirements. First, technical specifications will be defined with the CFP partner. Then, a fast modal analysis code as well as a more complex solver of the linearized Euler equations will be used to assess the impedance that maximizes the acoustic damping of the set of cut-on modes in the target range of frequency. A sheared flow profile in a cylindrical duct will be considered. Next, an optimisation procedure will be carried out to find the locally reacting liners whose impedance law fits at best the target impedance in the whole range of frequency. An attenuation of at least 10dB will be aimed at. For this, appropriate semi-empiricals models from the literature linking the geometrical features of the liners to their impedance will be used. This will allow the selection of five concepts of acoustic treatments, which will then be manufactured and tested in laboratory, with a grazing flow up to M=0.3. The impedance will be obtained by direct in-situ methods or by applying an eduction procedure from pressure measurements. This experimental impedance will then be used as an input for the numerical propagation code, to predict the expected attenuation in the industrial configuration. This will allow the selection of the best two concepts. Finally, large-scale prototypes of the two chosen liners will be manufactured and provided to the CFP partner for tests in the industrial configuration. An analysis for integration of proposals solutions in an industrial context will also be performed. Especially, issues about costs and weight and operating constraints will be dealt with.'

Introduzione (Teaser)

Over the past decades, technology has helped to make aircraft significantly quieter, by understanding and reducing the various components of engine noise. Now, EU-funded researchers seek a solution for acoustic liners to reduce noise generated by the air conditioning system and increase passengers' comfort.

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