Minimum environmental impact ultra-efficient cores for aircraft propulsion.

Información del proyecto

MINIMAL

Identificador del acuerdo de subvención: 101056863

DOI

10.3030/101056863

Fecha de la firma de la CE 3 Mayo 2022

Fecha de inicio 1 Septiembre 2022

Fecha de finalización 31 Agosto 2026

Financiado con arreglo a

• Climate, Energy and Mobility

Coste total

€ 3 527 276,00

Aportación de la UE

€ 3 527 276,00

Coordinado por

CHALMERS TEKNISKA HOGSKOLA AB
Sweden

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 (3)

Data management plan (DMP)

Develop a detailed data management plan based on the EC template and as outlined in Section 1.2.5related to task 6.3

Plan for the dissemination and exploitation including communication activities

The plan for dissemination and exploitation including communication will be extended from the content of the proposal and will serve as working document throughout the project duration.related to task 5.1

Air traffic and fleet modelling for 2050

The deliverable summarises the results from the air traffic forecast and fleet modelling work of Task 1.1 for the time horizon 2050. In the report, future air travel demand trends are identified, described, and quantified, with a specific focus on discussing possible future demand shifts related to the COVID-19 crisis and changing environmental perceptions. By employing BHLs fleet model, the report will show – for different scenarios – how air traffic volumes, fleet compositions, and the introduction of new aircraft influence global fuel burn by commercial aviation.related to taks 1.1

Websites, patent fillings, videos etc. (1)

MINIMAL public web site & social media

AI will develop a project website on the MINIMAL project's corporate design and provide content based on partners' input.Use of social media will be assessed and implemented if applicable related to task 5.1

Publicaciones

Conference proceedings (8)

Analysis of Free Piston Composite Cycle Engine Performance

Autores: E. Kulaksizoglu, T. Eker, A. Gangoli Rao, F. Yin
Publicado en: 2024
Editor: Delft University of Technology

Development of a Heat Transfer Model for a Free Double Piston and Identification of Thermal Management Challenges

Autores: Konstantinos Fotis, Zinon Vlahostergios, Dimitrios Misirlis, Kyros Yakinthos
Publicado en: EASN 2024, 2025
Editor: MDPI
DOI: 10.3390/ENGPROC2025090045

Heat transfer model development for a four stroke Piston engine concept

Autores: K. Fotis, Z. Vlahostergios, D. Misirlis, K. Yakinthos
Publicado en: FLOW 2024 - 12th Panhellenic Conference on Fluid Flow Phenomena, Thessaloniki, 15-16 April 2024, 2024
Editor: N/A

Assessing Nacelle Drag Increment: Implications of New Engine Technologies on Aircraft Performance

Autores: Odysseas Ziogas, Spyridon Antoniou, Pericles Panagiotou, Kyros Yakinthos
Publicado en: EASN 2024, 2025
Editor: MDPI
DOI: 10.3390/ENGPROC2025090049

Development of a Hydrogen Fuel Tank Design Model for Aero Engine Applications

Autores: V. Karaikos, Z. Vlahostergios, D. Misirlis, K, Yakinthos
Publicado en: FLOW 2024 - 12th Panhellenic Conference on Fluid Flow Phenomena, Thessaloniki, 15-16 April 2024, 2024

Conceptual Design Exploration of Hydrogen Enhanced Intercooling for Future Aeroengines

Autores: Petter Miltén, Isak Jonsson, Anders Lundbladh, Carlos Xisto
Publicado en: Volume 1: Aircraft Engine; Ceramics and Ceramic Composites, 2025
Editor: American Society of Mechanical Engineers
DOI: 10.1115/GT2025-152723

HEAT TRANSFER MODEL DEVELOPMENT FOR THE FREE DOUBLE PISTON ENGINE CONCEPT

Autores: K. Fotis, Z. Vlahostergios, D. Misirlis, K. Yakinthos
Publicado en: Proceedings of Global Power and Propulsion Society, 2024, ISSN 2504-4400
Editor: GPPS

PERFORMANCE ANALYSIS OF A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE

Autores: A. Johansson, P. Miltén, A. Lundbladh, C. Xisto
Publicado en: Proceedings of the 34th Congress of the International Council of the Aeronautical Sciences (ICAS 2024), 2024, ISSN 2958-4647
Editor: ICAS (International Council of the Aeronautical Sciences)

Peer reviewed articles (5)

Compact Heat Exchangers With Curved Fins for Hydrogen Turbofan Intercooling

Autores: Alexandre Capitao Patrao, Isak Jonsson, Carlos Xisto
Publicado en: Journal of Engineering for Gas Turbines and Power, Edición 146, 2024, ISSN 0742-4795
Editor: ASME International
DOI: 10.1115/1.4065887

Conceptual Design Exploration of Hydrogen Enhanced Intercooling for Future Aeroengines

Autores: Petter Miltén, Isak Johnsson, Anders Lundbladh, Carlos Xisto
Publicado en: Journal of Engineering for Gas Turbines and Power, Edición 147, 2025, ISSN 0742-4795
Editor: ASME International
DOI: 10.1115/1.4069483

Effect of Engine Design Parameters on the Climate Impact of Aircraft: A Case Study Based on Short-Medium Range Mission

Autores: Harjot Singh Saluja, Feijia Yin, Arvind Gangoli Rao, Volker Grewe
Publicado en: Aerospace 2023, 2023, ISSN 2226-4310
Editor: mdpi
DOI: 10.3390/aerospace10121004

A comprehensive well-to-wake climate impact assessment of sustainable aviation fuel

Autores: Luc Boerboom, Arvind Gangoli Rao, Volker Grewe, Feijia Yin
Publicado en: Scientific Reports, Edición 15, 2025, ISSN 2045-2322
Editor: Springer Science and Business Media LLC
DOI: 10.1038/S41598-025-13445-X

Generalized Method for the Conceptual Design of Compact Heat Exchangers

Autores: Petter Miltén, Isak Johnsson, Anders Lundbladh, Carlos Xisto
Publicado en: Journal of Engineering for Gas Turbines and Power, Edición 146, 2024, ISSN 0742-4795
Editor: ASME International
DOI: 10.1115/1.4065922