Hybrid Electric Regional Wing Integration Novel Green Technologies - HERWINGT

Información del proyecto

HERWINGT

Identificador del acuerdo de subvención: 101102010

DOI

10.3030/101102010

Fecha de la firma de la CE 9 Diciembre 2022

Fecha de inicio 1 Enero 2023

Fecha de finalización 31 Octubre 2026

Financiado con arreglo a

• Climate, Energy and Mobility

Coste total

€ 28 278 745,23

Aportación de la UE

€ 21 791 729,98

Coordinado por

AIRBUS DEFENCE AND SPACE SA
Spain

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

Data Management Plan (1)

Data Management Plan

Data management methodology for all data sets that will be handled throughout the project. First version of the document (M3)

Documents, reports (3)

Project Management and Quality Assurance Plan

Project Plan document describing the proper procedures towards the quality assurance of the project

Final Assessment Report of SAFs Compatibility and further activities required

Summary of compatibility studies between SAF pathways

Plan for Dissemination & Exploitation including communication activities

The concrete strategy that will be followed regarding the Dissemination Communication and Exploitation Activities will be elaborated at the beginning of the project and will be monitored and updated throughout the entire project life cycle

Publicaciones

Conference proceedings (7)

Aero-Structural Design Optimization of a Morphing Aileron Considering Actuation Aspects

Autores: Vittorio Cavalieri, Alessandro De Gaspari, Sergio Ricci
Publicado en: AIAA SCITECH 2024 Forum, 2024
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-2113

Aeroelastic Tailoring of a Strut-Braced Wing for a Medium Range Aircraft

Autores: Xavier Carrillo, Roeland De Breuker, Jurij Sodja
Publicado en: AIAA SCITECH 2024 Forum, 2024
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-2590

Aerodynamic design of a compliant morphing flap for the next generation hybrid-electric regional aircrafts

Autores: Francesco Antonio D'Aniello, Pietro Catalano, D. Quagliarella, and Mauro Minervino
Publicado en: 14th European Aeronautics Science Network (EASN) International Conference, 2025
Editor: EASN
DOI: 10.5281/zenodo.14717267

Conceptual Design and Topology Optimization of a Compliant Morphing Flap for Next Generation Hybrid-Electric Regional Aircraft

Autores: Maria Chiara Noviello, Ignazio Dimino, Salvatore Ameduri, Antonio Concilio
Publicado en: 2024
Editor: ICAS
DOI: 10.5281/zenodo.14930442

Multi–objective design optimization of a morphing aileron for a hybrid electric regional aircraft

Autores: Alessandro De Gaspari, Vittorio Cavalieri, Matteo Corti, and Sergio Ricci (POLIMI)
Publicado en: 34th Congress of the International Council of the Aeronautical Sciences (ICAS) Congress,, 2024
Editor: ICAS
DOI: 10.5281/zenodo.14930343

Aero-Structural Design of a High-Aspect Ratio Wing

Autores: Pietro Catalano, Gianluca Diodati, Davide Lucariello, Pier Luigi Vitagliano
Publicado en: AIAA AVIATION FORUM AND ASCEND 2024, 2024
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-3502

Aerodynamic Noise Prediction of Strut-Braced Wing Aircraft

Autores: Emanuele Sticchi, Daniele Ragni, Damiano Casalino, Francesco Avallone
Publicado en: 30th AIAA/CEAS Aeroacoustics Conference (2024), 2024
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-3012