HYdrogen eLectrical Engine Novel Architecture

Projektinformationen

HYLENA

ID Finanzhilfevereinbarung: 101137583

DOI

10.3030/101137583

EK-Unterschriftsdatum 23 November 2023

Startdatum 1 Januar 2024

Enddatum 30 Juni 2027

Finanziert unter

• Climate, Energy and Mobility

Gesamtkosten

€ 4 871 243,75

EU-Beitrag

€ 4 871 243,75

Koordiniert durch

AIRBUS
France

CORDIS bietet Links zu öffentlichen Ergebnissen und Veröffentlichungen von HORIZONT-Projekten.

Links zu Ergebnissen und Veröffentlichungen von RP7-Projekten sowie Links zu einigen Typen spezifischer Ergebnisse wie Datensätzen und Software werden dynamisch von OpenAIRE abgerufen.

Leistungen

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 (6)

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)

Validated parameterized state-of-the-art SOFC stack model

Delivery of a parameterized state of the art SOFC stack model to be used in WP3. The model is validated by means of experimental stack testing performed at DLR.

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.

Veröffentlichungen

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

Autoren: 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
Veröffentlicht in: 2024, ISSN 1025-9090
Herausgeber: 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

Autoren: P. Köhler, J. Tillner, S. Kabelac
Veröffentlicht in: 2024
Herausgeber: Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2024
DOI: 10.25967/630197

Other (1)

Update of down-selection of Concepts

Autoren: P. Köhler, J. Hollmann
Veröffentlicht in: 2024
Herausgeber: CORDIS - EU research results