Minimum environmental impact ultra-efficient cores for aircraft propulsion.

Informacje na temat projektu

MINIMAL

Identyfikator umowy o grant: 101056863

DOI

10.3030/101056863

Data podpisania przez KE 3 Maja 2022

Data rozpoczęcia 1 Września 2022

Data zakończenia 31 Sierpnia 2026

Finansowanie w ramach

• Climate, Energy and Mobility

Koszt całkowity

€ 3 527 276,00

Wkład UE

€ 3 527 276,00

Koordynowany przez

CHALMERS TEKNISKA HOGSKOLA AB
Sweden

CORDIS oferuje możliwość skorzystania z odnośników do publicznie dostępnych publikacji i rezultatów projektów realizowanych w ramach programów ramowych HORYZONT.

Odnośniki do rezultatów i publikacji związanych z poszczególnymi projektami 7PR, a także odnośniki do niektórych konkretnych kategorii wyników, takich jak zbiory danych i oprogramowanie, są dynamicznie pobierane z systemu OpenAIRE .

Rezultaty

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

Publikacje

Conference proceedings (8)

Analysis of Free Piston Composite Cycle Engine Performance

Autorzy: E. Kulaksizoglu, T. Eker, A. Gangoli Rao, F. Yin
Opublikowane w: 2024
Wydawca: Delft University of Technology

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

Autorzy: Konstantinos Fotis, Zinon Vlahostergios, Dimitrios Misirlis, Kyros Yakinthos
Opublikowane w: EASN 2024, 2025
Wydawca: MDPI
DOI: 10.3390/ENGPROC2025090045

Heat transfer model development for a four stroke Piston engine concept

Autorzy: K. Fotis, Z. Vlahostergios, D. Misirlis, K. Yakinthos
Opublikowane w: FLOW 2024 - 12th Panhellenic Conference on Fluid Flow Phenomena, Thessaloniki, 15-16 April 2024, 2024
Wydawca: N/A

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

Autorzy: Odysseas Ziogas, Spyridon Antoniou, Pericles Panagiotou, Kyros Yakinthos
Opublikowane w: EASN 2024, 2025
Wydawca: MDPI
DOI: 10.3390/ENGPROC2025090049

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

Autorzy: V. Karaikos, Z. Vlahostergios, D. Misirlis, K, Yakinthos
Opublikowane w: 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

Autorzy: Petter Miltén, Isak Jonsson, Anders Lundbladh, Carlos Xisto
Opublikowane w: Volume 1: Aircraft Engine; Ceramics and Ceramic Composites, 2025
Wydawca: American Society of Mechanical Engineers
DOI: 10.1115/GT2025-152723

HEAT TRANSFER MODEL DEVELOPMENT FOR THE FREE DOUBLE PISTON ENGINE CONCEPT

Autorzy: K. Fotis, Z. Vlahostergios, D. Misirlis, K. Yakinthos
Opublikowane w: Proceedings of Global Power and Propulsion Society, 2024, ISSN 2504-4400
Wydawca: GPPS

PERFORMANCE ANALYSIS OF A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE

Autorzy: A. Johansson, P. Miltén, A. Lundbladh, C. Xisto
Opublikowane w: Proceedings of the 34th Congress of the International Council of the Aeronautical Sciences (ICAS 2024), 2024, ISSN 2958-4647
Wydawca: ICAS (International Council of the Aeronautical Sciences)

Peer reviewed articles (5)

Compact Heat Exchangers With Curved Fins for Hydrogen Turbofan Intercooling

Autorzy: Alexandre Capitao Patrao, Isak Jonsson, Carlos Xisto
Opublikowane w: Journal of Engineering for Gas Turbines and Power, Numer 146, 2024, ISSN 0742-4795
Wydawca: ASME International
DOI: 10.1115/1.4065887

Conceptual Design Exploration of Hydrogen Enhanced Intercooling for Future Aeroengines

Autorzy: Petter Miltén, Isak Johnsson, Anders Lundbladh, Carlos Xisto
Opublikowane w: Journal of Engineering for Gas Turbines and Power, Numer 147, 2025, ISSN 0742-4795
Wydawca: 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

Autorzy: Harjot Singh Saluja, Feijia Yin, Arvind Gangoli Rao, Volker Grewe
Opublikowane w: Aerospace 2023, 2023, ISSN 2226-4310
Wydawca: mdpi
DOI: 10.3390/aerospace10121004

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

Autorzy: Luc Boerboom, Arvind Gangoli Rao, Volker Grewe, Feijia Yin
Opublikowane w: Scientific Reports, Numer 15, 2025, ISSN 2045-2322
Wydawca: Springer Science and Business Media LLC
DOI: 10.1038/S41598-025-13445-X

Generalized Method for the Conceptual Design of Compact Heat Exchangers

Autorzy: Petter Miltén, Isak Johnsson, Anders Lundbladh, Carlos Xisto
Opublikowane w: Journal of Engineering for Gas Turbines and Power, Numer 146, 2024, ISSN 0742-4795
Wydawca: ASME International
DOI: 10.1115/1.4065922