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CORDIS

Development of a Sensor with WIde Spectrum Sensitivity for MOnitoring of Damage and Defects In Composite Structures

Description du projet

Une caméra miniature sensible pour détecter les dommages et les défauts des structures composites des avions

Des impacts sur la structure composite d’un avion peuvent occasionner un délaminage ailleurs sur l’avion. Pour l’instant, la seule façon de détecter le délaminage consiste à procéder à des inspections régulières qui nécessitent d’immobiliser l’avion. Pour remédier à ce manque d’outils de diagnostic efficaces, le projet SWISSMODICS, financé par l’UE, cherche à développer une caméra miniature ultra-mince qui peut être incorporée dans la structure composite de l’avion où il existe un risque de délaminage. La caméra, qui sera sensible aux rayons X ainsi qu’à la lumière visible et infrarouge, facilitera les diagnostics, réduira le temps d’immobilisation et permettra d’établir des diagnostics en vol. Le projet constituera une avancée dans le domaine des tests non destructifs sur les avions.

Objectif

"Shocks on a composite structure of an aircraft can propagate and generate delamination at a distant place. There is currently no other method than regular inspection of the structure to detect these delamination, which requires to immobilize the aircraft. The SWISSMODICS project ambitions to answer the lack of efficient diagnostic tools by providing a miniature, ultra-thin camera to be incorporated in the composite structure of an aircraft where delamination risk to occur. This will considerably facilitate diagnostic and reduce immobilization time, even allowing in-operation diagnostic.

The SWISSMODICS project will develop a camera sensitive to X-ray, visible and infrared light. This will be achieved by creating a monolithic detector made of a CMOS pixel array with configurable pixels to the specificity of each wavelength range, covalently bonded to an absorber with areas sensitive to these 3 different wavelength ranges. The detector will be tested on a panel of section of fuselage in composite, with delamination defects representative of real defects.

The work will be executed by a consortium of 3 companies with complementary competences. CSEM, in Switzerland will develop the CMOS integrated circuit. G-ray, also in Switzerland, will develop the absorber with areas sensitive to different wavelength ranges and will perform wafer to wafer covalent bonding between the CMOS wafer and the absorber wafer. Finally, Almay, a French engineering company with experience in composites for the aeronautical applications, will provide guidance and will integrate and validate the detector on composite structures with defects.

This new sensor will be a breakthrough in non-destructive testing and will open the door to ""intelligent"" composite structures. In aeronautics, it will not only reduce immobilization time but also enable to reduce the security margin on composite parts thanks to continuous monitoring, resulting in economy of weight and fuel.
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Coordinateur

CSEM CENTRE SUISSE D'ELECTRONIQUE ET DE MICROTECHNIQUE SA - RECHERCHE ET DEVELOPPEMENT
Contribution nette de l'UE
€ 790 387,00
Adresse
RUE JAQUET DROZ 1
2000 Neuchatel
Suisse

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Région
Schweiz/Suisse/Svizzera Espace Mittelland Neuchâtel
Type d’activité
Research Organisations
Liens
Coût total
€ 790 387,00

Participants (3)