DEMONSTRATE
Financiado
DEMonstration Of Novel fuSelage sTructuRAl inTEgrity
DEMONSTRATE will realise an adaptable test rig, suitable for the full-scale testing of aircraft curved panels of variable geometry, at increased accuracy, reliability and cost-efficiency, through the advancement of innovative metr...
DEMONSTRATE will realise an adaptable test rig, suitable for the full-scale testing of aircraft curved panels of variable geometry, at increased accuracy, reliability and cost-efficiency, through the advancement of innovative metrology technologies, simulation and optimisation, as well as application of innovative but cost-effective methodologies to reduce uncertainty, cost and time on aeronautical sub-components testing.
The objective of DEMONSTARTE, aligned to the ‘Innovative light metallic and thermoplastic airframe section full scale testing’ (JTI-CS2-2020-CFP11-AIR-03-10) topic is the full-scale testing of three airframe section demonstrators, two metallic and a thermoplastic fuselage panel with an integrated stiffening structure, to demonstrate their structural integrity, supported by advanced simulation methodologies correlated with experimental data.
A number of enabling technologies have been planned to be developed and matured within the duration of the project, which will result to the realisation of an efficient, reliable and cost-effective test bench suitable for the full-scale testing of curved aeronautical panels, including:
the development of a virtual testing methodology for the definition of the stiffened panels boundary and loading conditions; the further development of an innovative, cost-efficient, easily adaptable fuselage panel full-scale test bench concept; the development and/or adaptation of a wide range of novel measurement techniques; the development and application of advanced simulation methodologies.
The developed test bench will be used for the execution of static tests on advanced metallic and thermoplastic curved integrally stiffened full-scale panels, representative of a business jet fuselage structure and the execution of an endurance test on an integrally stiffened 4th generation Al-Li curved panel.
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Duración del proyecto: 30 meses
Fecha Inicio: 2020-12-03
Fecha Fin: 2023-06-30
Fecha Fin: 2023-06-30
Línea de financiación: concedida
El organismo H2020 notifico la concesión del proyecto el día 2023-06-30
Línea de financiación objetivo
El proyecto se financió a través de la siguiente ayuda:
Presupuesto
El presupuesto total del proyecto asciende a
2M€
Líder del proyecto
LGAI TECHNOLOGICAL CENTER
Prestacion de servicios de ensayo, analisis, calibraje, innovacion tecnologica, control de calidad, homologacion, certificacion, inspeccion...
Perfil tecnológico
TRL
4-5
2M
Perfil tecnológico
TRL
4-5
2M
448.13K€ |
Participante