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TRIMIS

imProved reliabIlity inspeCtion of Aeronautic structure through Simulation Supported POD

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€7 462 969
EU Contribution
€4 957 469
Project website
Project Acronym
PICASSO
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Safety/Security,
Societal/Economic issues
Transport sectors
Passenger transport,
Freight transport

Overview

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

With ageing engines and the expected increase of air traffic in the next 20 years, a central challenge in the aeronautical industry will concern the increase of efficiency in maintenance which still represents around 20% of an operator's indirect operating costs. This challenge is particularly important for metallic parts within the engine and aircraft industry. Maintenance is directly related to the concept of Probability of Detection ("POD") curves which are obtained by expensive experimental campaigns.

Furthermore, the aeronautics regulations and expectations regarding safety are increasing. New aeronautic regulations require appropriate damage tolerance assessments for critical parts (for example compressor and turbine disc), to address the potential for failure from material, manufacturing and service induced anomalies within the Approved Life of the part.

Objectives

The concept of using Non Destructive Testing ('NDT'), using low cost simulations to obtain POD curves, will be evaluated within the PICASSO project.

The aim of PICASSO was to build a new and original concept of 'simulation supported POD curves, based on NDT simulation in addition to existing experimental data bases'. The main objectives of the PICASSO project were to increase the accuracy, and reduce the cost of, a POD campaign with NDT simulation techniques.

Methodology

This was achieved by:

  • Completing experimental NDT inspections by simulated NDT inspections: suppressing the needs of manufacturing expensive samples with defects;
  • More representative samples of the population for the POD campaign: enhancing the accuracy of the POD samples and increasing their numbers thanks to simulation techniques;
  • Delta POD approach: suppressing the need of a new POD campaign for similar parts or inspection configurations.

The main impacts of the project are:

  • To improve the answer to FAA/EASA damage tolerance requirements with higher knowledge and accuracy on NDT inspection PODs;
  • Savings in costs, concerning aircraft maintenance and engine development.

Funding

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

Results

At this moment (early February 2013) no final results have been presented or have been published. The results mentioned are therefore based on preliminary information.

The main results of the PICASSO project are the validation of the concept of 'simulation-supported POD' by way of initial realistic results, robust methodologies and endorsed implementation rules. Through realistic industrial applications, design offices and maintenance departments will benefit from a clear overview of the potential impacts.

Methodology recommendations obtained as a result of the project on simulation supported POD determination will enable to establish the basis and recommendations for a future European standard for qualification and reliability of inspection for the aircraft industry.

The intensive use of simulation supported POD and the development of a future EU standard, will be the future.

Strategy targets

Innovating for the future (technology and behaviour): A European Transport Research and Innovation Policy

Partners

Lead Organisation
Organisation
Safran Aircraft Engines
Address
2 Bvd Du General Martial-Valin, 75724 Paris, France
EU Contribution
€548 584
Partner Organisations
Organisation
Mtu Aero Engines
Address
Dachauer Strasse 665, 80995 MUENCHEN, Germany
Organisation website
EU Contribution
€279 125
Organisation
Frauenhofer Geselschaft Zur Foerderung Der Angewandten Forschung E.v.
Address
Hansastrasse 27C, 80686 MUNCHEN, Germany
Organisation website
EU Contribution
€422 200
Organisation
Commissariat A L Energie Atomique Et Aux Energies Alternatives
Address
RUE LEBLANC 25, 75015 PARIS 15, France
Organisation website
EU Contribution
€759 020
Organisation
Safran Helicopter Engines
Address
Avenue Du President Szydlowski, 64510 Bordes, France
EU Contribution
€154 355
Organisation
Technic Control
Address
ANDRZEJA ANTOSIEWICZA 1, 71 642 SZCZECIN, Poland
Organisation website
EU Contribution
€226 467
Organisation
Airbus
Address
2 ROND POINT EMILE DEWOITINE, 31700 BLAGNAC, France
Organisation website
EU Contribution
€304 333
Organisation
Phi-Meca Engineering
Address
Centre D'affaire Du Zenit L'arche, Rue De Sarlieve 34, 63800 Cournon-D'auvergne, France
EU Contribution
€317 995
Organisation
Bundesanstalt Fuer Materialforschung Und -Pruefung
Address
Unter Den Eichen 87, 12205 Berlin, Germany
Organisation website
EU Contribution
€444 660
Organisation
Gkn Aerospace Sweden Ab
Address
46181 Trollhaettan, Sweden
EU Contribution
€264 252
Organisation
Rolls Royce Plc
Address
65 Buckingham gate, LONDON, SW1E 6AT, United Kingdom
Organisation website
EU Contribution
€157 300
Organisation
Ruag Space Germany Gmbh
Address
AM GLASWERK 6, 01640 COSWIG, Germany
Organisation website
EU Contribution
€258 725
Organisation
Twi Limited
Address
Granta Park Great Abington, Cambridge, CB1 6AL, United Kingdom
EU Contribution
€377 380
Organisation
Chalmers Tekniska Hoegskola Ab
Address
41296 GOTHENBURG, Sweden
Organisation website
EU Contribution
€443 073

Technologies

Technology Theme
Non destructive testing
Technology
New NDT and repair methods for ALM parts
Development phase
Research/Invention

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