Investigation and Maturation of Technologies for Hybrid Electric Propulsion

Informazioni relative al progetto

IMOTHEP

ID dell’accordo di sovvenzione: 875006

DOI

10.3030/875006

Progetto chiuso

Data della firma CE 11 Dicembre 2019

Data di avvio 1 Gennaio 2020

Data di completamento 30 Giugno 2024

Finanziato da

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Costo totale

€ 18 675 947,50

Contributo UE

€ 10 392 845,00

Coordinato da

OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
France

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 (19)

CDAP

CDAP (M12, M18, M36) Task 7.3

Synthesis of ASS-LA battery technology evaluation

Synthesis of the ASSLA battery technology evaluation report Task 42

Synthesis of benefits of HEP for regional and SMR aircraft

Synthesis of benefits of HEP for regional and SMR aircraft Task 1.5

Thrust/drag bookkeeping methods comparative assessment on BLI

Thrust/drag bookkeeping methods comparative assessment on BLI Task 2.5

Gap analysis and preliminary roadmap on HEP development

Technology gaps - Preliminary synthesis Task 6.1

Synthesis on Integrated Vehicle Design
Need for infrastructures for the development of HEP

Need for infrastructures for the development of HEP Task 6.2

Synthesis on AeroPropulsive design
Synthesis on Electrical Architecture
Synthesis on Energy Generation
Synthesis on Electric components
L2 Architecture Evaluation and Lessons Learned

L2 Architecture Evaluation and Lessons LearnedTask 3.2

ATM and airport challenges of hybrid electric aircraft integration

ATM and airport challenges of hybrid electric aircraft integration Task 6.3

Final battery model documentation

Final battery model Task 42

Certification issues and regulatory evolutions for HEP

Certification issues and regulatory evolutions for HEP Task 6.3

Assessment of design and sizing logic for Hybrid Electric aircraft

Assessment of design and sizing logic for Hybrid Electric aircraftTask 1.2

Certification noise assessment of optimized configurations

Certification noise assessment of optimized configurations Task 2.6

Fuel cells feasibility study

Fuel cells feasibility study Task 4.3

Roadmap for the development of hybrid electric propulsion

Roadmap for the development of hybrid electric propulsion Task 6.4

Websites, patent fillings, videos etc. (4)

IMOTHEP Final brochure

IMOTHEP Final brochureTask 7.3

Project electronic newsletter (6-monthly)

Project electronic newsletter (ideally 6-monthly, at least once a year) Task 7.1

project video

project video Task 7.2

Dissemination set (poster, leaflet, Kakemono) and Website

Dissemination set (poster, leaflet, Kakemono) and Website Task 7.1

Other (1)

Project consortium identity (logo, graph. Chart)

Project consortium identity logo graph ChartTask 71

Pubblicazioni

Conference proceedings (20)

Design and Comparison of High-speeds PMSM and IM for Aircraft Application

Autori: Dahnoun Larbi, Fontchastagner Julien, Mezani Smaïl, Takorabet Noureddine, Viguier Christophe
Pubblicato in: 2023 IEEE Transportation Electrification Conference and Expo, Asia-Pacific (ITEC Asia-Pacific), Numero -, 2024, Pagina/e -
Editore: IEEE
DOI: 10.1109/itecasia-pacific59272.2023.10372325

Conceptual design of a blended wing body aircraft with distributed electric propulsion

Autori: Wim Lammen, Jos Vankan
Pubblicato in: Proceedings of MEA2021 - More Electric Aircraft Conference, 20-21/10/21, Bordeaux (FR), https://web2.see.asso.fr/mea2021, 2021
Editore: MEA

Development of an aerodynamic analysis tool for boundary layer ingestion concept design

Autori: Xin Zhao, Carlos Xisto, Shia-Hui Peng
Pubblicato in: Proceedings of 33rd Congress of the International Council of the Aeronautical Sciences (ICAS2022), 4-9 Sept 2022, Stockholm, Sweden, https://icas2022.com/, 2022
Editore: ICAS

Low-fidelity Aerodynamic Integration of Distributed Electric Propulsion on a Blended Wing Body including Boundary Layer Ingestion

Autori: V.J.E. Aalbers, J. van Muijden
Pubblicato in: Proceedings of 9th EUCASS-3AF - 27/6-1/7/22, Lille (FR), https://eucass-3af-2022.eu/, 2022
Editore: EUCASS-3AF
DOI: 10.13009/eucass2022-6105

Sizing superconducting motor associated with cryogenics power electronics for disruptive hybrid electric propulsion aircrafts

Autori: Jean Lévêque, Rémi Dorget, Min Zhang, Abdelrahman Elwakee, Christophe Viguier, Sabrina Ayat
Pubblicato in: Proceedings of 9th EUCASS-3AF - 27/6-1/7/22, Lille (FR), https://eucass-3af-2022.eu/, 2022
Editore: EUCASS-3AF
DOI: 10.13009/eucass2022-7234

Propeller predesign for distributed propulsion architectures

Autori: Y. Maldonado, L. Delcambre and B. Rodriguez
Pubblicato in: Proceedings of Towards Sustainable Aviation Summit - TSAS 2022, 18-20 Oct, 2022 Toulouse (FR), https://www.3af-tsas.com/, 2022
Editore: TSAS

Reduced Computational Burden of Modulated Model-Predictive Control for Synchronous Reluctance Motor Drive Applications

Autori: Jacopo Riccio, Petros Karamanakos, Michele Degano, Chris Gerada, Pericle Zanchetta
Pubblicato in: 2023 IEEE Energy Conversion Congress and Exposition (ECCE), Numero -, 2024, Pagina/e 4995-5002, ISBN 979-8-3503-1644-5
Editore: IEEE
DOI: 10.1109/ecce53617.2023.10362110

Multiphysics modeling and optimization of PMSM for high speed operation

Autori: Thomas Marcand, Charles-Henri Bonnard, Smail Mezani, Noureddine Takorabet
Pubblicato in: 2023 IEEE International Magnetic Conference - Short Papers (INTERMAG Short Papers), Numero -, 2023, Pagina/e 1-2
Editore: IEEE International
DOI: 10.5281/zenodo.12579817

Performances of direct drive and magnetically geared PMSMs with different cooling technologies

Autori: Smail Mezani, Thomas Marcand, Charles-Henri Bonnard, Noureddine Takorabet
Pubblicato in: 2024 IEEE International Magnetic Conference - Short Papers (INTERMAG Short Papers), Numero -, 2024, Pagina/e -
Editore: IEEE International
DOI: 10.5281/zenodo.12580005

Power Management and Fault Analysis Hybrid Propulsion Aircraft System

Autori: Vergori Cesare, Manzo Marco Maria, Civardi Massimo, Dirk Zimmer, Kenny Fong
Pubblicato in: Proceedings of 9th EUCASS-3AF - 27/6-1/7/22, Lille (FR), https://eucass-3af-2022.eu/, 2022
Editore: EUCASS-3AF
DOI: 10.13009/eucass2022-7313

Sizing Electrical Machines Using OpenOffice Calc

Autori: MEZANI Smaïl, BELGUERRAS Walid, TAKORABET Noureddine and LUBIN Thierry
Pubblicato in: Proceedings of 9th EUCASS-3AF - 27/6-1/7/22, Lille (FR), https://eucass-3af-2022.eu/, 2022
Editore: EUCASS-3AF
DOI: 10.13009/eucass2022-6110

IMOTHEP European project : an investigation of hybrid electric propulsion for commercial aircraft

Autori: Philippe Novelli, Sébastien Defoort, N. Tantot, Dirk Zimmer, Dario Varchetta, Christophe Viguier, Pia Iodice
Pubblicato in: Proceedings of AIAA Aviation Forum, 2023, Pagina/e 1-19
Editore: AIAA
DOI: 10.2514/6.2023-4131

Study of a Regional Turboprop Aircraft with Electrically Assisted Turboshaft

Autori: Anaïs Luisa Habermann, Moritz Georg Kolb,Philipp Maas, Hagen Kellermann, Carsten Rischmüller, Fabian Peter and Arne Seitz
Pubblicato in: Aerospace, Numero 10(6), 2023, Pagina/e 529
Editore: MDPI
DOI: 10.3390/aerospace10060529

First order thermal analysis methodology for hybridelectric propelled aircraft in early design stage

Autori: Van Muijden, J.; Aalbers V.J.E.
Pubblicato in: Proceedings of Aerospace Europe Conference 2023 – 10TH EUCASS – 9TH CEAS, Numero 1, 2023
Editore: EUCASS-CEAS
DOI: 10.5281/zenodo.8271919

Design and performance evaluation of a full turboelectric distributed electric propulsion aircraft: preliminary results of EU project IMOTHEP

Autori: E. NGUYEN VAN, S. DEFOORT, K. FONG, M. RIDEL, D. DONJAT, P. CHOY, C. VIGUIER, M. ALI, T. YOUSSEF
Pubblicato in: Proceedings of 9th EUCASS-3AF - 27/6-1/7/22, Lille (FR), https://eucass-3af-2022.eu/, 2022
Editore: EUCASS-3AF
DOI: 10.13009/eucass2022-6134

Parametric Study of the Noise Emitted by Uncorrelated, Distributed, Electric Fans

Autori: Sebastien Guerin; Antoine Moreau; Robert Meier zu Ummeln; Martin Staggat
Pubblicato in: Proceedings of AIAA 2021 Aviation Forum, 2-6 August 2021, Washington (USA), Numero 18, 2021
Editore: AIAA
DOI: 10.2514/6.2021-2137

Design and performances of a turbo-electric and Distributed Propulsion aircraft in the Small and Medium Range segment: intermediate results from the European project IMOTHEP

Autori: Eric Nguyen Van, Sebastien Defoort, Christophe Viguier, Smail Mezani, Noureddine Takorabet, Jesúz Sainz
Pubblicato in: Proceedings of AIAA 2024 SciTech, 8-12/1/24 in Orlando, FL, USA, 2024
Editore: AIAA
DOI: 10.5281/zenodo.11918733

Conceptual design study for a radical short-medium range hybrid aircraft

Autori: Vankan, Jos; Lammen, Wim; Defoort, Sebastien
Pubblicato in: Proceedings of 9th EUCASS-3AF - 27/6-1/7/22, Lille (FR), https://eucass-3af-2022.eu/, Numero 16, 2022, Pagina/e -
Editore: EUCASS-3AF
DOI: 10.13009/eucass2022-6103

Thermal management principal analysis of hybrid electric aircraft with turboelectric propulsion using distributed propulsors

Autori: van Muijden J.; Aalbers V.J.E.
Pubblicato in: Proceedings of 9th EUCASS-3AF - 27/6-1/7/22, Lille (FR), https://eucass-3af-2022.eu/, 2022
Editore: EUCASS-3AF
DOI: 10.5281/zenodo.7031204

Multidisciplinary Design and Optimization of the Blended Wing Body Configuration SMILE

Autori: Julie Gauvrit-Ledogar, Arnault Tremolet, Sébastien Defoort, Franck Morel, Romain Liaboeuf, Michaël Méheut
Pubblicato in: Proceedings of 9th EUCASS-3AF - 27/6-1/7/22, Lille (FR), https://eucass-3af-2022.eu/, 2022
Editore: EUCASS-3AF
DOI: 10.13009/eucass2022-6061

Peer reviewed articles (6)

Aerodynamic Investigation of the High-Lift Performance of a Propeller-Driven Regional Transport Aircraft with Distributed Propulsion

Autori: Dennis Keller
Pubblicato in: Journal Physics: Conference Series, Numero 2526, 2023, Pagina/e 012007
Editore: IOP Publishing Ltd
DOI: 10.1088/1742-6596/2526/1/012007

Are batteries fit for hybrid-electric regional aircraft?

Autori: Helmut Kühnelt, Francesco Mastropierro, Ningxin Zhang, Somayeh Toghyani, Ulrike Krewer
Pubblicato in: Journal of Physics: Conference Series, Numero 2526, 2023, Pagina/e 12026
Editore: IOP Publishing Ltd
DOI: 10.1088/1742-6596/2526/1/012026

Aerodynamic Effects of a Wing Surface Heat Exchanger

Autori: Habermann Anaïs; Khot Ankit; Lampl David; Perren Christof
Pubblicato in: Aerospace, Numero 10 (5), 2023, Pagina/e 407
Editore: MDPI
DOI: 10.3390/aerospace10050407

A contribution to the investigation of acoustic interferences in aircraft distributed propulsion

Autori: Sébastien Guérin; Damiano Tormen
Pubblicato in: CAES Aeronautical Journal, Numero 14, 2023, Pagina/e 965-982, ISSN 1869-5582
Editore: Springer Science + Business Media
DOI: 10.1007/s13272-023-00679-6

Model-Based Design of High Energy All-Solid-State Li Batteries with Hybrid Electrolytes

Autori: Somayeh Toghyani; Florian Baakes; Ningxin Zhang; Helmut Kühnelt; Walter Cistjakov; Ulrike Krewer
Pubblicato in: Journal of the Electrochemical Society, Numero Volume 169, Number 4, 2022, Pagina/e 040550, ISSN 0013-4651
Editore: Electrochemical Society, Inc.
DOI: 10.1149/1945-7111/ac653b

Conceptual Design of Solid-State Li-Battery for Urban Air Mobility

Autori: S. Toghyani; W. Cistjakov; F. Baakes; U. Krewer
Pubblicato in: Journal of The Electrochemical Society, 170 (10), Art.-Nr.: 103510, Numero 1, 2023, ISSN 1945-7111
Editore: IOP Publishing Ltd
DOI: 10.1149/1945-7111/ad00de

Other (1)

Modelling, simulation and optimization methodologies for low-emission aircraft concepts

Autori: W.J. Vankan W.F. Lammen E.H. Baalbergen
Pubblicato in: NLR internal report NLR-TP-2021-415, 2021
Editore: -