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Fibre Reinforced thermoplAstics Manufacturing for stiffEned, complex, double curved Structures.

Project description

Innovative thermoplastic composites for next-generation fuselage

The fuselage of the next generation of Large Passenger Aircraft (LPA) is currently being assessed and could take advantage of thermoplastic composites (TPC). Besides their intrinsic properties benefits, TPC have the potential to fill the gap between current and forecasted production rates. However, TPC production faces significant challenges, in particular manufacturing complex geometries of high quality. As an alternative to thermosets, the EU-funded FRAMES project will explore a manufacturing approach for an integral thermoplastic rear-end fuselage with critical design features. The project will rely on an intelligent heating system, efficient manufacturing processes for stiffeners and a self-heated tool, introducing an innovative double-curved and thick skin co-consolidation process, with its entire stiffening structure in one shot.

Objective

The fuselage of the next generation of Large Passenger Aircrafts´ (LPA) will be made with thermoplastic (TP) composites. In fact, even if this kind of materials are being increasingly used in aerospace industry, as they contribute to lighter aircrafts and consequently to fuel consumption reduction, there are still some issues to be overcome until this becomes a reality.
The manufacturing complex forms of rear end section with continuous fibre-reinforced TP still poses a considerable challenge: higher processing temperatures and raw material costs, need of complex temperature-controlled tooling, etc. Automated fibre placement (AFP) is a workable alternative for more complicated TP Composites (TPC) shapes with varying part thickness (e.g. fuselage shells, wing and stabilizer torsion boxes and stringers), but one of the challenges is void removal, which is more difficult with TP than with thermosets.
FRAMES aims to fully define technical and cost performance of an optimized integral TP rear end manufacturing process with critical design features as an alternative to thermoset materials. Thanks to a self-heated tool with process driven heating zones and advanced lay up process simulation, FRAMES will be capable of predicting heating law for efficient TP-AFP, correlated with lay-up trials, mastering TP-stiffeners manufacturing process, optimizing co-consolidation cycle. Its main innovation relies on the co-consolidation of a double curved and thick skin with its entire stiffening structure in one shot.
FRAMES will support the spread of alternative heating process for thermoplastic AFP by developing a simulation tool able to predefine processing parameters of the most common aerospace grades thermoplastics. At the end, the advanced rear end (ARE) concept that will allow the savings (NRC and maintenance costs, higher integration level at lighter weight, etc.) will be easily applicable to other panels or structures with the same interface principle or same architecture

Coordinator

ECOLE SUPERIEURE DES TECHNOLOGIES INDUSTRIELLES AVANCEES
Net EU contribution
€ 113 728,75
Address
ALLEE FAUSTE D ELHUYAR 90
64210 Bidart
France

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SME

The organization defined itself as SME (small and medium-sized enterprise) at the time the Grant Agreement was signed.

Yes
Region
Nouvelle-Aquitaine Aquitaine Pyrénées-Atlantiques
Activity type
Higher or Secondary Education Establishments
Links
Total cost
€ 113 728,75

Participants (3)