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Virtual evaluation and robust detection for engine component non destructive testing

Virtual evaluation and robust detection for engine component non destructive testing

Objective

The VERDICT proposal is aimed at specifying, testing, developing and validating new modeling tools for Non Destructive Testing of aircraft engine parts. The main results are user friendly interfaced modeling tools coupled with CAD commonly used by aerospace engine manufacturers, and fitted with designer and inspector needs. With these tools, time to market and cost of aircraft engines should be reduced by a.voiding design/manufacturing/inspection iterations during engine development, and a balance between part weight, bursting risk and inspection cost should be optimized for critical parts.

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Coordinator

SNECMA SA

Address

Bd. Du GÉNÉRal Martial Valin, 2
75724 Paris

France

Administrative Contact

Pierre THOURAUD (Mr)

Participants (13)

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CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE

France

CITY UNIVERSITY

United Kingdom

COMMISSARIAT A L'ENERGIE ATOMIQUE

France

DIPL. PHYS. M. KAEMMERER SYSTEMFORSCHUNG

Germany

ECOLE SUPÉRIEURE D'ELECTRICITÉ - SUPELEC

France

FRAUNHOFER-GESELLSCHAFT ZUR FOERDERUNG DER ANGEWANDTEN FORSCHUNG E.V.

Germany

MTU AERO ENGINES GMBH

Germany

ROLLS ROYCE PLC

United Kingdom

TECHSPACE AERO SA

Belgium

TURBOMECA SA

France

TZFP GBR

Germany

UNIVERSITE DE LIEGE

Belgium

UNIVERSITE DE PARIS-SUD XI

France

Project information

Grant agreement ID: G4RD-CT-2002-00860

  • Start date

    1 February 2003

  • End date

    31 January 2006

Funded under:

FP5-GROWTH

  • Overall budget:

    € 5 460 562

  • EU contribution

    € 2 974 012

Coordinated by:

SNECMA SA

France