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TRIMIS

“Test Methods for analySis OF Infusion pAnels” (SOFIA)

PROJECTS
Funding
European
European Union
Duration
-
Status
Ongoing
Geo-spatial type
Other
Total project cost
€639 496
EU Contribution
€498 340
Project Acronym
SOFIA
STRIA Roadmaps
Transport mode
Airborne icon
Transport policies
Other specified
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP11-2020-01
Link to CORDIS
Background & Policy context

Novel infusion techniques could have different implications than classical pre-preg technologies. To increase the robustness in the early design and subsequent certification phases of the component is a challenge. Confidence in this technology must be tackled with the analysis and development of new test methods.

Objectives

The EU-funded SOFIA project will develop advanced test methods to evaluate the performance of innovative infusion techniques in finished aerospace components. Models will facilitate analytical characterisation of component behaviours and failure modes.

Methodology

To comply with this task, the project is focused on three main levels:

  • A presizing of the component as the initial phase to determine the expected failure modes (FM). This step is the basis to evaluate the behavior of the component under applied loads (combined loading state) and the definition of Level 2 and 3 tests
  • Level 2 is the characterization of the FM. The first step is to define these expected mechanical FM that will be analyzed. This phase has a significant importance as the classical mechanisms of failure associated with the use of pre-pregs may be altered by the new infusion manufacturing process. The test plan definition, tooling design and manufacturing, mathematical approaches to be used, test execution and the correlation of the analytical results (developed FEM and / or mathematical laws to predict behavior) with real test results are the main tasks of this stage. This failure mode characterization is the basis for the definition of the behavior of the subcomponent for the next stage.
  • Level 3 is the validation of the analytical characterization of the FM and the subcomponent global behaviour. Non-linear FEM with cohesive elements and virtual crack closure technique will be developed. The numerical predictions, the test plan definition, tooling design and manufacturing, test execution and the correlation of the expected results vs real test results, are the main tasks of this stage.

In addition to this project, if necessary, the topic manager will be offered the possibility for the manufacturing of complementary coupons at any stage of the project.

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.
Other Programme
JTI-CS2-2020-CFP11-AIR-03-11 Development and execution of new test methods for thermoset panel manufactured in an automated tape layup of dry unidirectional fibres (UD) or non-crimped fabrics (NCF) and subsequent infusion

Partners

Lead Organisation
Organisation
Alestis Aerospace Sl
Address
CALLE INGENIERO RAFAEL RUBIO ELOLA AEROPOLIS, 41309 LA RINCONADA SEVILLA, Spain
EU Contribution
€217 455
Partner Organisations
Organisation
Lgai Technological Center Sa
Address
Campus Universidat Autonoma De Barcelona Facultad De Medicina, 8193 Cerdanyola Barcelona, Spain
Organisation website
EU Contribution
€111 911
Organisation
Universidad De Sevilla
Address
Calle S. Fernando 4, 41004 Sevilla, Spain
EU Contribution
€168 974

Technologies

Technology Theme
Manufacturing processes
Technology
Smart composite manufacture
Development phase
Validation
Technology Theme
Computer-aided design and engineering
Technology
Predictive virtual testing of composite structures up to failure
Development phase
Validation

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