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

Informazioni relative al progetto

HOPE

ID dell’accordo di sovvenzione: 101096275

DOI

10.3030/101096275

Data della firma CE 7 Dicembre 2022

Data di avvio 1 Febbraio 2023

Data di completamento 31 Gennaio 2027

Finanziato da

• Climate, Energy and Mobility

Costo totale

€ 3 394 197,50

Contributo UE

€ 3 394 197,50

Coordinato da

TECHNISCHE UNIVERSITEIT DELFT
Netherlands

CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.

I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .

Risultati finali

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.

Pubblicazioni

Conference proceedings (10)

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

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

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

Autori: Payyappalli, Manas; Frehe, Gijs; Yin, Feijia; Gangoli Rao, Arvind
Editore: 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

Autori: Luca Nicola Quaroni, Tomas Sinnige, Roberto Merino-Martinez
Pubblicato in: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editore: 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

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

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

Autori: Luca Nicola Quaroni, Roberto Merino-Martinez, Fernanda d. Monteiro and S. Satish Kumar
Pubblicato in: 30th AIAA/CEAS Aeroacoustics Conference (2024), Numero AIAA 2024-3209, 2024
Editore: 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

Autori: Battiston, A., Magrini, A., Ponza, R., Benini, E., Türkyilmaz, B., Seitz, A., & Heidebrecht, A.
Pubblicato in: 2024
Editore: ICAS 2024 Conference Proceedings

Adapting turbofan noise modelling tool using neural networks

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

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

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

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

Autori: Kolb, Moritz Georg; Seitz, Arne; Türkyilmaz, Barlas; Ma, Yiyuan; Hornung, Mirko
Pubblicato in: 2024
Editore: ICAS Conference proceedings

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

Autori: Luca Nicola Quaroni, Roberto Merino-Martinez
Pubblicato in: AIAA AVIATION FORUM AND ASCEND 2025, 2025
Editore: 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

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

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

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

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

Autori: Kaushal Dave, Sarah Link, Francesca De Domenico, Ferry Schrijer, Fulvio Scarano, Arvind Gangoli Rao
Pubblicato in: Fuel Communications, Numero 23, 2025, ISSN 2666-0520
Editore: 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

Autori: Barlas Türkyilmaz, Michael Lüdemann, Moritz Georg Kolb, Alexandros Lessis
Pubblicato in: Aerospace, Numero 12, 2025, ISSN 2226-4310
Editore: MDPI AG
DOI: 10.3390/AEROSPACE12070585

Other (1)

HOPE leaflet (Trifold)

Autori: Ergon Research
Pubblicato in: 2024
Editore: ERGON Italy
DOI: 10.5281/ZENODO.13582990