Hybrid Electric Regional Wing Integration Novel Green Technologies - HERWINGT

Informations projet

HERWINGT

N° de convention de subvention: 101102010

DOI

10.3030/101102010

Date de signature de la CE 9 Decembre 2022

Date de début 1 Janvier 2023

Date de fin 31 Octobre 2026

Financé au titre de

• Climate, Energy and Mobility

Coût total

€ 28 278 745,23

Contribution de l’UE

€ 21 791 729,98

Coordonné par

AIRBUS DEFENCE AND SPACE SA
Spain

CORDIS fournit des liens vers les livrables publics et les publications des projets HORIZON.

Les liens vers les livrables et les publications des projets du 7e PC, ainsi que les liens vers certains types de résultats spécifiques tels que les jeux de données et les logiciels, sont récupérés dynamiquement sur OpenAIRE .

Livrables

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 (4)

Enablers for Multi-Functional LE design
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

Publications

Conference proceedings (9)

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

Auteurs: Vittorio Cavalieri, Alessandro De Gaspari, Sergio Ricci
Publié dans: AIAA SCITECH 2024 Forum, 2024
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-2113

The Aerodynamic Design of a Compliant Morphing Flap for Next-Generation Hybrid Electric Regional Aircraft

Auteurs: Francesco Antonio D’Aniello, Pietro Catalano, Domenico Quagliarella, Mauro Minervino
Publié dans: EASN 2024, 2025, ISSN 2673-4591
Éditeur: MDPI
DOI: 10.3390/ENGPROC2025090013

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

Auteurs: Xavier Carrillo, Roeland De Breuker, Jurij Sodja
Publié dans: AIAA SCITECH 2024 Forum, 2024
Éditeur: 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

Auteurs: Francesco Antonio D'Aniello, Pietro Catalano, D. Quagliarella, and Mauro Minervino
Publié dans: 14th European Aeronautics Science Network (EASN) International Conference, 2025
Éditeur: EASN
DOI: 10.5281/zenodo.14717267

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

Auteurs: Maria Chiara Noviello, Ignazio Dimino, Salvatore Ameduri, Antonio Concilio
Publié dans: 2024
Éditeur: ICAS
DOI: 10.5281/zenodo.14930442

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

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

Aero-Structural Design of a High-Aspect Ratio Wing

Auteurs: Pietro Catalano, Gianluca Diodati, Davide Lucariello, Pier Luigi Vitagliano
Publié dans: AIAA AVIATION FORUM AND ASCEND 2024, 2024
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-3502

AI-Based Generative Algorithms Applied to the Design of Blended Wing Body Aircraft

Auteurs: Marta A. Martín, Andrés Mateo, Thomas Wagenaar, Gonzalo Rubio, Sven A. Lanzan Ferran
Publié dans: AIAA AVIATION FORUM AND ASCEND 2025, 2025, ISSN 0001-1452
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-3292

Aerodynamic Noise Prediction of Strut-Braced Wing Aircraft

Auteurs: Emanuele Sticchi, Daniele Ragni, Damiano Casalino, Francesco Avallone
Publié dans: 30th AIAA/CEAS Aeroacoustics Conference (2024), 2024
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-3012

Peer reviewed articles (2)

Design and Optimization of a Compliant Morphing Trailing Edge for High-Lift Generation

Auteurs: Salvatore Ameduri, Bernardino Galasso, Maria Chiara Noviello, Ignazio Dimino, Antonio Concilio, Pietro Catalano, Francesco Antonio D’Aniello, Giovanni Marco Carossa, Laurent Pinazo, John Derry, Britney Biju, Shruthi Shreedharan
Publié dans: Applied Sciences, Numéro 15, 2025, ISSN 2076-3417
Éditeur: MDPI AG
DOI: 10.3390/APP15052529

Design optimization and virtual testing of a morphing aileron with high actuation bandwidth

Auteurs: Vittorio Cavalieri, Alessandro De Gaspari
Publié dans: Aerospace Science and Technology, Numéro 168, 2025, ISSN 1270-9638
Éditeur: Elsevier BV
DOI: 10.1016/J.AST.2025.111110