Hydrogen Optimized multi-fuel Propulsion system for clean and silEnt aircraft

Información del proyecto

HOPE

Identificador del acuerdo de subvención: 101096275

DOI

10.3030/101096275

Fecha de la firma de la CE 7 Diciembre 2022

Fecha de inicio 1 Febrero 2023

Fecha de finalización 31 Enero 2027

Financiado con arreglo a

• Climate, Energy and Mobility

Coste total

€ 3 394 197,50

Aportación de la UE

€ 3 394 197,50

Coordinado por

TECHNISCHE UNIVERSITEIT DELFT
Netherlands

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

Documents, reports (5)

Design, testing & emission analysis of multi-fuel combustor at atmospheric pressure

This deliverable will report the design of a multi-fuel combustor at atmospheric pressure. Accordingly, the testing will be conducted. This design will be essential for numerical simulations to extract the inputs for reactor network models in D2.2.

Final Report on the BLI propulsor design and performance properties

This deliverable will report the full-scale design of the aft BLI propulsor and evaluate the acoustic characteristics of the designed propulsor to identify the low noise configuration. The resulting parametric geometry will be an input for T1.1 and the experimental work in WP3.

Multi-reactor high fidelity chemical kinetics model

This deliverable will present the multi-reactor network designs and the details chemical kinetics for analysing the emissions of the combustor designed in HOPE.

Mid-term dissemination and exploitation assessment and report

The communication and exploitation activities in the first half of the project duration will be summarised in this report. Their success will be assessed according to the criteria defined in the PEDR.

Final report on multi-fuel power plant system design and performance models

This deliverable will report the conceptual design of the multi-fuel propulsion system in HOPE and the characteristics of such propulsion system.

Websites, patent fillings, videos etc. (1)

Project website

The project website will be one of the key channels for HOPE to communicate the project activities and research findings.

Publicaciones

Conference proceedings (10)

CFD-Based Scouting for the Design of a Multi-Fuel Kerosene/Hydrogen Atmospheric Burner

Autores: Palanti, L., Mazzei, L., Bianchini, C., Link, S., Dave, K., De Domenico, F., & Rao, A. G.
Publicado en: 2024
Editor: ICAS 2024 Conference Proceedings
DOI: 10.5281/ZENODO.14802717

The Validity of Schmidt-Appleman Criterion for Modern Turbofan Engines: A Numerical Study

Autores: Payyappalli, Manas; Frehe, Gijs; Yin, Feijia; Gangoli Rao, Arvind
Editor: owards Sustainable Aviation Summit 2025
DOI: 10.5281/ZENODO.19221282

Investigation of Noise Generation by a Model-Propeller in Turbulent Inflow Through Advanced Signal Processing Techniques

Autores: Luca Nicola Quaroni, Tomas Sinnige, Roberto Merino-Martinez
Publicado en: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-3147

Psychoacoustic Characterization Of An Isolated Propeller At Different Inflow Turbulence Conditions And Collective Pitch Angles

Autores: Roberto Merino-Martinez, Luca Nicola Quaroni
Publicado en: Proceedings of the 11th Convention of the European Acoustics Association Forum Acusticum / EuroNoise 2025, 2025
Editor: European Acoustics Association
DOI: 10.61782/FA.2025.0711

Collective blade pitch angle effect on grid turbulence ingestion noise by an isolated propeller

Autores: Luca Nicola Quaroni, Roberto Merino-Martinez, Fernanda d. Monteiro and S. Satish Kumar
Publicado en: 30th AIAA/CEAS Aeroacoustics Conference (2024), Edición AIAA 2024-3209, 2024
Editor: AIAA - American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-3209

Design Optimisation of a Boundary Layer Ingestion Propulsor for a Multi-Fuel Hydrogen Aircraft

Autores: Battiston, A., Magrini, A., Ponza, R., Benini, E., Türkyilmaz, B., Seitz, A., & Heidebrecht, A.
Publicado en: 2024
Editor: ICAS 2024 Conference Proceedings

Adapting turbofan noise modelling tool using neural networks

Autores: null null, Chenzhao Li, Evangelia Maria Thoma, null null
Publicado en: Proceedings of Global Power & Propulsion Society, 2025
Editor: GPPS
DOI: 10.33737/GPPS25-TC-014

Mitigation Strategies For Acoustic Reflections Generated By An Axisymmetric Wind Tunnel Nozzle

Autores: Luca Nicola Quaroni, Roberto Merino-Martinez
Publicado en: Proceedings of the 11th Convention of the European Acoustics Association Forum Acusticum / EuroNoise 2025, 2025
Editor: European Acoustics Association
DOI: 10.61782/FA.2025.0571

Modelling and Initial Assessment of a Fuel Cell Auxiliary Propulsion and Power Unit (Presentation)

Autores: Kolb, Moritz Georg; Seitz, Arne; Türkyilmaz, Barlas; Ma, Yiyuan; Hornung, Mirko
Publicado en: 2024
Editor: ICAS Conference proceedings

Aeroacoustic Characterization of Acoustically-Treated Turbulence Grids in Axisymmetric Contraction for Open-Jet Wind Tunnels

Autores: Luca Nicola Quaroni, Roberto Merino-Martinez
Publicado en: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-3688

Peer reviewed articles (4)

Human response to the noise emissions of an isolated propeller under turbulent inflow conditions

Autores: Roberto Merino-Martinez, Luca Nicola Quaroni
Publicado en: INTER-NOISE and NOISE-CON Congress and Conference Proceedings, Edición 272, 2025, ISSN 0736-2935
Editor: Institute of Noise Control Engineering (INCE)
DOI: 10.3397/IN_2025_1076063

Assessment of multi-fuel powered turbofans: Performance, dimensions and emissions

Autores: Xin ZHAO, Tomas GRÖNSTEDT, Moritz G. KOLB
Publicado en: Chinese Journal of Aeronautics, 2026, ISSN 1000-9361
Editor: Elsevier BV
DOI: 10.1016/J.CJA.2026.104082

Kerosene-H2 blending effects on flame properties in a multi-fuel combustor

Autores: Kaushal Dave, Sarah Link, Francesca De Domenico, Ferry Schrijer, Fulvio Scarano, Arvind Gangoli Rao
Publicado en: Fuel Communications, Edición 23, 2025, ISSN 2666-0520
Editor: Elsevier BV
DOI: 10.1016/J.JFUECO.2025.100139

Design of a Short-To-Medium-Range Baseline Aircraft with an Entry into Service in 2035 for the HOPE Project

Autores: Barlas Türkyilmaz, Michael Lüdemann, Moritz Georg Kolb, Alexandros Lessis
Publicado en: Aerospace, Edición 12, 2025, ISSN 2226-4310
Editor: MDPI AG
DOI: 10.3390/AEROSPACE12070585

Other (1)

HOPE leaflet (Trifold)

Autores: Ergon Research
Publicado en: 2024
Editor: ERGON Italy
DOI: 10.5281/ZENODO.13582990