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TRIMIS

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

PROJECTS
Funding
European
European Union
Duration
-
Status
Ongoing
Geo-spatial type
Other
Total project cost
€923 172
EU Contribution
€923 172
Project Acronym
SWISSMODICS
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Safety/Security
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP10-2019-01
Link to CORDIS
Objectives

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.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.1.

Partners

Lead Organisation
Organisation
Csem Centre Suisse D'electronique Et De Microtechnique Sa - Recherche Et Developpement
Address
Rue Jaquet Droz 1, 2002 Neuchatel, Switzerland
EU Contribution
€470 172
Partner Organisations
Organisation
Almay Technologies
Address
37 Rue de Peuron, 86300 CHAUVIGNY, France
EU Contribution
€52 375
Organisation
G Ray Nanobonding Sarl
Address
ROUGES TERRES 61, 2068 HAUTERIVE, Switzerland
EU Contribution
€400 625

Technologies

Technology Theme
Composite materials
Technology
Composite fuselage sections
Development phase
Research/Invention
Technology Theme
Sensor technologies
Technology
Integrated sensors for structural components
Development phase
Research/Invention

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