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Hybrid Electric Regional Wing Integration Novel Green Technologies - HERWINGT

Descrizione del progetto

Volare alto con una nuova progettazione alare

L’industria aeronautica sta imboccando un percorso per affrontare i propri impatti sull’ambiente e sul clima. Migliorare le prestazioni ambientali del settore è tra le priorità principali e l’UE sta investendo in tecnologie e processi chiave per rendere i velivoli a impatto zero una realtà. L’aviazione regionale dovrebbe portare approcci nuovi e innovativi alle operazioni relative ad aeromobili e trasporto aereo I veicoli aerei che volano lungo distanze inferiori a 500 km (connessioni regionali) beneficeranno delle tecnologie di propulsione ibrida-elettrica. In questo contesto, il progetto HERWINGT, finanziato dall’UE, svilupperà tecnologie chiave per occuparsi di una nuova progettazione alare per un velivolo regionale ibrido elettrico. Seguirà la produzione, l’assemblaggio, i concetti e i processi strutturali, gli studi di concetto, nonché i compromessi in termini di configurazione e architettura per un componente alare completo.

Obiettivo

Development of key technologies to address a new wing design for a HER aircraft maturing up to TRL5: manufacturing, assembly, structural concepts and processes, concept studies, configuration and architecture trade offs for a full wing component are part of the activity. As a physical demonstration concept, the detail design and manufacturing of the relevant components of a centre wing section of a HER Aircraft will be addressed.

Conceptual wing studies: configuration and architecture (structural arrangement, Systems allocation and disposition, flight control system) trade offs for a full wing. Full wing structural arrangement mock up for innovative wing concepts, Structural and Multidisciplinary Optimization studies for definition of the optimal structural configuration of wing.

Demonstration platform: wingbox, high lift devices, control surfaces, load alleviation devices focusing on the centre section as a demonstration platform:
- Integrated Centre section wing box structure with the inner Propulsion stage: Full span (pylon to pylon) torsion box concept representative of more ambitious tip 2 tip concept. Multispar concept, Access manholes and panels, Sustainable aviation fuel and Integrated Fuel vent systems.
- Inner section Leading Edges, Integrated Inductive ice protection system integration, Multifunctionality: erosion, impact, Lightning, ice protection, Morphing concepts, Functional tests, Bird strike tests (virtual or real)
- Inner section Flap and high lift solutions: Integrated flap solutions. Multifunctionality application to flap.

Key processing technologies: Low cost-high integrated out of autoclave technologies. Dry fiber placement and liquid resin infusion for integrated multispar torsion box. Thermoplastic composites processing: In situ consolidation for integrated flap skin and Leading edge applications. Thermoplastic welding and co-consolidation for Integration. Bonding technologies exploration towards certifiable solutions.

Parole chiave

Coordinatore

AIRBUS DEFENCE AND SPACE SA
Contribution nette de l'UE
€ 5 100 826,85
Indirizzo
calle Aviocar nº2
28906 GETAFE (MADRID)
Spagna

Mostra sulla mappa

Regione
Comunidad de Madrid Comunidad de Madrid Madrid
Tipo di attività
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Collegamenti
Costo totale
€ 8 011 858,00

Partecipanti (31)

Partner (1)