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

Projektinformationen

HOPE

ID Finanzhilfevereinbarung: 101096275

DOI

10.3030/101096275

EK-Unterschriftsdatum 7 Dezember 2022

Startdatum 1 Februar 2023

Enddatum 31 Januar 2027

Finanziert unter

• Climate, Energy and Mobility

Gesamtkosten

€ 3 394 197,50

EU-Beitrag

€ 3 394 197,50

Koordiniert durch

TECHNISCHE UNIVERSITEIT DELFT
Netherlands

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Leistungen

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.

Veröffentlichungen

Conference proceedings (10)

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

Autoren: Palanti, L., Mazzei, L., Bianchini, C., Link, S., Dave, K., De Domenico, F., & Rao, A. G.
Veröffentlicht in: 2024
Herausgeber: ICAS 2024 Conference Proceedings
DOI: 10.5281/ZENODO.14802717

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

Autoren: Payyappalli, Manas; Frehe, Gijs; Yin, Feijia; Gangoli Rao, Arvind
Herausgeber: 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

Autoren: Luca Nicola Quaroni, Tomas Sinnige, Roberto Merino-Martinez
Veröffentlicht in: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Herausgeber: 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

Autoren: Roberto Merino-Martinez, Luca Nicola Quaroni
Veröffentlicht in: Proceedings of the 11th Convention of the European Acoustics Association Forum Acusticum / EuroNoise 2025, 2025
Herausgeber: European Acoustics Association
DOI: 10.61782/FA.2025.0711

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

Autoren: Luca Nicola Quaroni, Roberto Merino-Martinez, Fernanda d. Monteiro and S. Satish Kumar
Veröffentlicht in: 30th AIAA/CEAS Aeroacoustics Conference (2024), Ausgabe AIAA 2024-3209, 2024
Herausgeber: 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

Autoren: Battiston, A., Magrini, A., Ponza, R., Benini, E., Türkyilmaz, B., Seitz, A., & Heidebrecht, A.
Veröffentlicht in: 2024
Herausgeber: ICAS 2024 Conference Proceedings

Adapting turbofan noise modelling tool using neural networks

Autoren: null null, Chenzhao Li, Evangelia Maria Thoma, null null
Veröffentlicht in: Proceedings of Global Power & Propulsion Society, 2025
Herausgeber: GPPS
DOI: 10.33737/GPPS25-TC-014

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

Autoren: Luca Nicola Quaroni, Roberto Merino-Martinez
Veröffentlicht in: Proceedings of the 11th Convention of the European Acoustics Association Forum Acusticum / EuroNoise 2025, 2025
Herausgeber: European Acoustics Association
DOI: 10.61782/FA.2025.0571

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

Autoren: Kolb, Moritz Georg; Seitz, Arne; Türkyilmaz, Barlas; Ma, Yiyuan; Hornung, Mirko
Veröffentlicht in: 2024
Herausgeber: ICAS Conference proceedings

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

Autoren: Luca Nicola Quaroni, Roberto Merino-Martinez
Veröffentlicht in: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Herausgeber: 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

Autoren: Roberto Merino-Martinez, Luca Nicola Quaroni
Veröffentlicht in: INTER-NOISE and NOISE-CON Congress and Conference Proceedings, Ausgabe 272, 2025, ISSN 0736-2935
Herausgeber: Institute of Noise Control Engineering (INCE)
DOI: 10.3397/IN_2025_1076063

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

Autoren: Xin ZHAO, Tomas GRÖNSTEDT, Moritz G. KOLB
Veröffentlicht in: Chinese Journal of Aeronautics, 2026, ISSN 1000-9361
Herausgeber: Elsevier BV
DOI: 10.1016/J.CJA.2026.104082

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

Autoren: Kaushal Dave, Sarah Link, Francesca De Domenico, Ferry Schrijer, Fulvio Scarano, Arvind Gangoli Rao
Veröffentlicht in: Fuel Communications, Ausgabe 23, 2025, ISSN 2666-0520
Herausgeber: 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

Autoren: Barlas Türkyilmaz, Michael Lüdemann, Moritz Georg Kolb, Alexandros Lessis
Veröffentlicht in: Aerospace, Ausgabe 12, 2025, ISSN 2226-4310
Herausgeber: MDPI AG
DOI: 10.3390/AEROSPACE12070585

Other (1)

HOPE leaflet (Trifold)

Autoren: Ergon Research
Veröffentlicht in: 2024
Herausgeber: ERGON Italy
DOI: 10.5281/ZENODO.13582990