HYSOP
Hybrid Silicide-Based Lightweight Components for Turbine and Energy Applications
| Coordinatore | OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Organization address
address: Avenue de la Division Leclerc 29 contact info |
| Nazionalità Coordinatore | France [FR] |
| Totale costo | 5˙895˙233 € |
| EC contributo | 4˙476˙047 € |
| Programma | FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics) |
| Code Call | FP7-AAT-2010-RTD-1 |
| Funding Scheme | CP-FP |
| Anno di inizio | 2010 |
| Periodo (anno-mese-giorno) | 2010-10-01 - 2015-03-31 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Organization address
address: Avenue de la Division Leclerc 29 contact info |
FR (CHATILLON) | coordinator | 1˙124˙820.00 |
| 2 |
THE UNIVERSITY OF BIRMINGHAM
Organization address
address: Edgbaston contact info |
UK (BIRMINGHAM) | participant | 794˙682.00 |
| 3 |
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE
Organization address
address: Rue Michel -Ange 3 contact info |
FR (PARIS) | participant | 512˙938.00 |
| 4 |
FRAUNHOFER-GESELLSCHAFT ZUR FOERDERUNG DER ANGEWANDTEN FORSCHUNG E.V
Organization address
address: Hansastrasse 27C contact info |
DE (MUENCHEN) | participant | 491˙602.00 |
| 5 |
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
DE (KOELN) | participant | 485˙230.00 |
| 6 |
Nome Ente NON disponibile
Organization address
city: Nancy contact info |
FR (Nancy) | participant | 252˙145.75 |
| 7 |
Karlsruher Institut fuer Technologie
Organization address
address: Kaiserstrasse 12 contact info |
DE (Karlsruhe) | participant | 243˙786.22 |
| 8 |
UNIVERSITE HENRI POINCARE NANCY 1
Organization address
address: Rue Lionnois 24-30 contact info |
FR (NANCY) | participant | 212˙722.25 |
| 9 |
L - UP SAS
Organization address
address: Avenue de Friedland 32 contact info |
FR (PARIS) | participant | 131˙115.00 |
| 10 |
TECHNISCHE UNIVERSITAET DARMSTADT
Organization address
address: Karolinenplatz 5 contact info |
DE (DARMSTADT) | participant | 127˙813.78 |
| 11 |
SNECMA SAS
Organization address
address: 2 Bvd du General Martial-Valin contact info |
FR (PARIS) | participant | 99˙192.00 |
Mappa
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Obiettivo del progetto (Objective)
'HYSOP’s goal is to develop solutions for manufacturing lightweight high temperature (HT) turbine components and to design new coating systems (protection against oxidation, water vapour and CMAS). Nb/Nb5Si3 and Si3N4/MoSi2 composites are lightweight HT materials (density < 6.5~7 and < 5.6 g/cm3, respect.) with application potential above 1300°C making them candidates for advanced aero-engine components, allowing reduction of fuel consumption, CO2 emissions and cooling air needs, hence a further increase in efficiency and reduction in engine weight. Though remarkable HT mechanical properties have been achieved (strength, creep), especially in the FP6 ULTMAT project, short/medium term application cannot be envisaged since improved oxidation resistance and optimised microstructures for enhanced mechanical properties are required. The partners (engine manufacturer, research centres, universities) will join their expertise to reach following objectives: - design static (vane, seal segment) and rotating (blade) components with tailored microstructures and properties, including superalloy/HT-material hybrid structures where superior performance is foreseen over monolithic material - develop the corresponding advanced routes for processing (based on powder metallurgy: net-shape HIPing, powder injection moulding, laser fabrication) and joining - design oxidation/corrosion resistant coating systems, based on expertise gained on substrate/coating/environment interactions on Nb-Si materials, superalloys and Environmental/Thermal Barrier Coatings; - test the coatings in service-like conditions: medium (~800°C) and high (1100-1300°C) temperatures in dry/wet air, corrosion by molten oxides, up to a burner rig test; - converge the two approaches in assessing the mechanical behaviour of bare and coated specimens; - finally, to propose a set of manufacturing and coating solutions for the HT materials for medium term application in aero- and small land-based turbines.'
Introduzione (Teaser)
Researchers are developing lightweight components for turbines along with tougher coating systems. Combining these innovations improves the efficiency and reliability of large-scale industrial structures.