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TRIMIS

DEMonstration Of Novel fuSelage sTructuRAl inTEgrity

PROJECTS
Funding
European
European Union
Duration
-
Status
Ongoing
Geo-spatial type
Other
Total project cost
€1 664 476
EU Contribution
€1 299 571
Project Acronym
DEMONSTRATE
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Safety/Security
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP11-2020-01
Link to CORDIS
Objectives

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.

Methodology

A number of enabling technologies have been planned to be developed and matured within the duration of the project, which will result in 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; and
  • 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.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.4. - ITD Airframe
Other Programme
JTI-CS2-2020-CFP11-AIR-03-10 Innovative light metallic and thermoplastic airframe section full scale testing

Partners

Lead Organisation
Organisation
Lgai Technological Center Sa
Address
Campus Universidat Autonoma De Barcelona Facultad De Medicina, 8193 Cerdanyola Barcelona, Spain
Organisation website
EU Contribution
€851 446
Partner Organisations
Organisation
Athina-Erevnitiko Kentro Kainotomias Stis Technologies Tis Pliroforias, Ton Epikoinonion Kai Tis Gnosis
Address
Artemedios 6 Kai Epidavrou 6, 151 25 Maroussi, Greece
Organisation website
EU Contribution
€448 125

Technologies

Technology Theme
Composite materials
Technology
Thermoplastic-based composite materials
Development phase
Demonstration/prototyping/Pilot Production

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