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CORDIS - Forschungsergebnisse der EU
CORDIS

Medium-range hybrid low-pollution flexi-fuel/hydrogen sustainable engine

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

Data Management Plan (öffnet in neuem Fenster)

Task 11 The DMP will provide the identification elements and the descriptions of the data sets and will include details regarding how the research data will be handled during theproject and how they will be preserved after it is completed Success indicator complete documentation ready and approved by the governing bodies of the project in agreement with the PO

Data Management Plan Update 1 (öffnet in neuem Fenster)

Task 1.2: Update of the Data Management Plan n.1 is released. Success indicator: report timely issued.

Project Handbook (öffnet in neuem Fenster)

Task 11 The Project Handbook brings together a wide range of general operational information including contact details roles and responsibilities of the partners according to the governance structure operational and reporting processes templates procedures for the preparation of deliverables Success indicator complete documentation ready and approved by the governing bodies of the project in agreement with the PO

Dissemination and Exploitation Plan (öffnet in neuem Fenster)

Task 1.3: The D&E plan will provide the details of Communication, Dissemination and Exploitation of the results. It will also contain the relevant KPIs established by the project governing bodies in agreement with the PO. Success indicator: complete documentation ready and approved by the governing bodies of the project in agreement with the PO.

Dissemination and Exploitation Plan Update1 (öffnet in neuem Fenster)

Task 1.3: Update of the Dissemination and Communication Report n.1 is released. Success indicator: report timely issued.

Fuel selection report (öffnet in neuem Fenster)

Task 6.2: Conventional fossil jet fuels as well as a range of sustainable jet fuels with a range of specifications covering a range of Cetane numbers between 17 and 80 will be selected and acquired. This range of jet fuels should include JetA1, JP5 and dodecane together, with a few low and high Cetane number (sustainable) jet fuels. Success indicator: fuels are documented and acquisition is successfully accomplished and documented.

Description of baseline combustor set- up (öffnet in neuem Fenster)

Task 6.1: A brief description of the combustor model to be used for experiments in WP6, numerical simulations in WP3 and hidden physics extraction in WP4 is isued. Success indicator: complete documentation is issued.

Reduced mechanism for SAF- blends (öffnet in neuem Fenster)

Task 2.1: The surrogate model and reduced mechanism for SAF blends and engine’s Chemical Reactor Network model for evaluation of pollutant emissions in conceptual design stage is use-ready. Success indicator: successful validation of reduced mechanism against detailed mechanism in laminar flames (premixed/non-premixed); Reaction-Network framework validated numerically against steady-state simulations of standard combustor design.

Chemistry-turbulence interaction model (öffnet in neuem Fenster)

Task 3.1: An experimentally validated improved turbulence-chemistry interaction model for variable fuel blends is delivered specifically for the efficiency-driven needs of scale-resolving simulations on Tier-0 HP-Clusters. Success indicator: improved speed-up and scalability (>5%) of computations in a canonic jet-flame configuration.

Minimal-fidelity model of reference engine (öffnet in neuem Fenster)

Task 23 Based on an available research engine configuration a small twinspool turbofan provided by the partnerLUND a first airframeengine matching and minimalfidelity design will be carried out based essentially onperformance parameters using conventional JetA fuels Success indicator minimalfidelity model validated against lowfidelity numerical simulations of the same configuration

Minimal-fidelity model of airframe (öffnet in neuem Fenster)

Task 2.2: Minimal-fidelity model of the selected airframe configuration and selection of mission conditions for a typical short-range flight is delivered. Sucess indicator: minimal fidelity model validated on the basis of existing data and procedures (e.g. JTI project).

Veröffentlichungen

Large Eddy Simulation of a Model Jet-Engine Swirl-Stabilized Flame Using Sustainable Aviation Fuels (öffnet in neuem Fenster)

Autoren: Pierre Vauquelin, Bora O. Cakir, David Sanned, Megha Prakash, Jan-Peter Hannappel, Arman A. Subash, Mattias Richter, Xue-Song Bai, Christer Fureby
Veröffentlicht in: AIAA SCITECH 2025 Forum, 2025
Herausgeber: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-0163

Thermodynamic Design of an Aeroengine for Sustainable Aviation Fuels with a Focus on 3D Components Conception: High Pressure Turbine (öffnet in neuem Fenster)

Autoren: Jan Donndorf, Federico Lo Presti, Francesca di Mare
Veröffentlicht in: European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, 16th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, 2025
Herausgeber: European Turbomachinery Society
DOI: 10.29008/ETC2025-271

Design, Simulation and Virtual Certification Assessment of a Medium Range Aeroengine Combustor (öffnet in neuem Fenster)

Autoren: Pierre Vauquelin, Jan Donndorf, Federico Lo Presti, Francesca di Mare, Xue-Song Bai, Christer Fureby
Veröffentlicht in: AIAA SCITECH 2026 Forum, 2026
Herausgeber: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2026-0745

Multidimensional Chemistry Coordinate Mapping for Large Eddy Simulations of a Turbulent Premixed Bluff-Body Burner (öffnet in neuem Fenster)

Autoren: Pierre Vauquelin, Yuchen Zhou, Arvid Åkerblom, Christer Fureby, Xue-Song Bai
Veröffentlicht in: AIAA SCITECH 2025 Forum, 2025
Herausgeber: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2025-2485

All Mach flows density-based / pressure-based coupling: method and preliminary results on the example of a rim seal flow in a one-stage axial turbine (öffnet in neuem Fenster)

Autoren: Federico Lo Presti, Francesca di Mare
Veröffentlicht in: European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, 16th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, 2025
Herausgeber: European Turbomachinery Society
DOI: 10.29008/ETC2025-272

Chemistry Mapping in Large-Eddy Simulations of Bluff-Body Flames Using Alternative Jet Fuels (öffnet in neuem Fenster)

Autoren: Pierre Vauquelin, Yuchen Zhou, Arvid Åkerblom, Christer Fureby, Xue-Song Bai
Veröffentlicht in: AIAA Journal, Ausgabe 64, 2026, ISSN 0001-1452
Herausgeber: American Institute of Aeronautics and Astronautics (AIAA)
DOI: 10.2514/1.J065789

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