REMFOS
"DESIGN, MANUFACTURING AND RELIABILITY EVALUATION OF EMBEDDED SENSOR"
| Coordinatore | FUNDACION TECNALIA RESEARCH & INNOVATION
Organization address
address: PARQUE TECNOLOGICO DE MIRAMON PASEO MIKELETEGI 2 contact info |
| Nazionalità Coordinatore | Spain [ES] |
| Totale costo | 79˙999 € |
| EC contributo | 59˙998 € |
| Programma | FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives |
| Code Call | SP1-JTI-CS-2009-01 |
| Funding Scheme | JTI-CS |
| Anno di inizio | 2010 |
| Periodo (anno-mese-giorno) | 2010-01-01 - 2011-01-31 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
FUNDACION TECNALIA RESEARCH & INNOVATION
Organization address
address: PARQUE TECNOLOGICO DE MIRAMON PASEO MIKELETEGI 2 contact info |
ES (DONOSTIA-SAN SEBASTIAN) | coordinator | 29˙994.00 |
| 2 |
FIBERSENSING-SISTEMAS AVANCADOS DEMONITORIZACAO SA
Organization address
address: RUA VASCONCELOS COSTA 277 contact info |
PT (MAIA) | participant | 30˙004.00 |
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Obiettivo del progetto (Objective)
'The objective of this activity is to design and manufacture composite specimens integrating fibre optic sensors, evaluate the reliability of the sensors, develop a concept to evaluate the system reliability and define a design of experiments of sensorized structures. The purpose of this study is to facilitate the validation of real-time health monitoring systems, which can detect strain as well as the temperature of the structure at multiple locations through numerous embedded optical fibre sensors. Optical fibre sensors for damage detection will be embedded in the structure made of carbon fibre reinforced plastic (CFRP) composite laminates. An integrated assessment of all critical manufacturing steps of fibre Bragg grating strain sensors will be performed in order to achieve high reliability of the embedding process in composite materials. The study will comprise the analysis of different types of optical fibres towards the optimization of embedding processes in composite materials. High resolution strain mapping by embedding series of closely spaced independent sensors in composite material samples will be assessed. Parameters that influence the infant failure of the structures will be analysed and the tests required to asses their effect will be defined. A preliminary test campaign based on thermal, mechanical and fatigue tests have already been defined.'
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INDUCER (2010)
Induction Heating and Health Monitoring Solutions for Smart Aircraft Maintenance using Adapted Composite Patches
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