HYdrogen eLectrical Engine Novel Architecture

Información del proyecto

HYLENA

Identificador del acuerdo de subvención: 101137583

DOI

10.3030/101137583

Fecha de la firma de la CE 23 Noviembre 2023

Fecha de inicio 1 Enero 2024

Fecha de finalización 30 Junio 2027

Financiado con arreglo a

• Climate, Energy and Mobility

Coste total

€ 4 871 243,75

Aportación de la UE

€ 4 871 243,75

Coordinado por

AIRBUS
France

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

Websites, patent fillings, videos etc. (1)

Project Website

A project website will be delivered, where information about the project and the partners will be collected and made public. Link to papers, patents, dissemination and exploitation activities will be included too.

Documents, reports (5)

Technical report on state-of-the-art SOFC response under operating conditions

Delivery of steady-state power density values for planar button cells based on State-of-the-Art Materials (commercial solid oxide cells) in standardized operating conditions.

Update of down-selection of Concepts

Subsequent to detailed thermodyamic cycle simulations and evaluation, a further down-selection is executed to choose the most promising cylces to be investigated in WP4 and WP5. The deliverable is public except some detail features that could be sensitive.

Demonstrator requirements specification

This deliverable will contain a list of requirements with the objectives to be achieved by the demonstrator as identified and cross-checked with the other WPs. The requirements specification will include purpose and scope of the test rig, stakeholder identification, rated operating conditions, expected off-design operating conditions, functional requirements, usability requirements, technical requirements (e.g. control, safety, integration), assumptions, constraints, dependencies and key performance metrics.

Final Component Modeling

Delivery of finalized propulsion system component models to be used in T3.4 and WP4-5. This includes turbomachinery, combustion chambers, electrical motor and power electronics as well as mechanical components.Deliverable is public except some special features that could be sensitive (or be kept internally to the consortium)

Conceptual Design Exploration

Report completing task T4.1 including the exploration of different SOFC-GT conceptual designs, a preliminary assessment of the identified concepts and a concept down-selection based on expert judgement.

Publicaciones

Peer reviewed articles (2)

Hydrogen-fueled Solid Oxide Fuel Cell-Gas Turbine (SOFC-GT) hybrid engines for aircraft propulsion: Comprehensive thermodynamic heat integration study

Autores: P. Köhler, J. Hollmann, S. Kabelac
Publicado en: Energy Conversion and Management: X, Edición 30, 2026, ISSN 2590-1745
Editor: Elsevier BV
DOI: 10.1016/J.ECMX.2026.101883

Future Highly Efficient Engines with Solid Oxide Fuel Cell–Gas Turbine Coupling: System Modeling Study and Comparison of Directly and Indirectly Coupled SOFC–GT Systems

Autores: Pascal Köhler, Jan Hollmann, Anis Taissir, Marc P. Heddrich, Stephan Kabelac
Publicado en: Aerospace, Edición 13, 2026, ISSN 2226-4310
Editor: MDPI
DOI: 10.3390/AEROSPACE13030263

Conference proceedings (2)

Hydrogen-Powered Solid Oxide Fuel Cell - Gas Turbine System for Aeronautical Application, 34th Congress of the International Council of the Aeronautical Sciences

Autores: D. Kierbel, T. Neuland, P.E. Roux, P. Nehter, J. Hollmann, C.N. Dagli, P. Köhler, S. Kabelac, A.G. Rao, F. de Domenica et al
Publicado en: 2024, ISSN 1025-9090
Editor: International Council of the Aeronautical Sciences

Thermodynamic Assessment of Hydrogen-Fueled Solid Oxide Fuel Cell - Gas Turbine (SOFC-GT) Systems for Low-Emission Aircraft Propulsion

Autores: P. Köhler, J. Tillner, S. Kabelac
Publicado en: 2024
Editor: Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2024
DOI: 10.25967/630197

Other (1)

Update of down-selection of Concepts

Autores: P. Köhler, J. Hollmann
Publicado en: 2024
Editor: CORDIS - EU research results