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HERWINGT

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Cerrado

Hybrid Electric Regional Wing Integration Novel Green Technologies HERWINGT

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... ver más

31/12/2025

AIRBUS DEFENCE AND...

28M€

Presupuesto del proyecto: 28M€

Líder del proyecto

AIRBUS DEFENCE AND SPACE Investigacion, estudio previo, proyecto, construccion, modificacion, mantenimiento y reparacion de aeronaves de todas clases para usos civil...

TRL 4-5 | 1M€

Fecha límite participación Sin fecha límite de participación.

Ver 33 Participantes

Financiación concedida El organismo HORIZON EUROPE notifico la concesión del proyecto el día 2022-12-09

HORIZON-JU-CLEAN-AVIATION-2022-01-HER-04: Innovative Wing Design for Hybrid-E... Objective:Design of an innovative and more efficient wing with relevant technology bricks matured to...

I+D +1

Cerrada hace 2 años

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Información adicional privada

No hay información privada compartida para este proyecto. Habla con el coordinador.

33 Participantes

AIRBUS DEFENCE AND SPACE

5.61M€ | Lider

TU Delft

1.14M€ | Participante

IKERLAN

350.58K€ | Participante

FOKKER AEROSTRUCTURES

911.00K€ | Participante

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Duración del proyecto: 36 meses Fecha Inicio: 2022-12-09
Fecha Fin: 2025-12-31

Líder del proyecto

AIRBUS DEFENCE AND SPACE Investigacion, estudio previo, proyecto, construccion, modificacion, mantenimiento y reparacion de aeronaves de todas clases para usos civil...

TRL 4-5 | 1M€

Presupuesto del proyecto 28M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto 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.

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