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IMOTHEP

Financiado

Cerrado

Investigation and Maturation of Technologies for Hybrid Electric Propulsion

To meet the goal of a carbon neutral growth of commercial aviation, the top level objective of IMOTHEP is to achieve a key step in assessing the potential offered by hybrid electric propulsion (HEP) and, ultimately, to build the... ver más

30/06/2024

ONERA

19M€

Presupuesto del proyecto: 19M€

Líder del proyecto

OFFICE NATIONAL DETUDES ET DE RECHERCHES AERO... No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

Ver 36 Participantes

Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2024-06-30

LC-MG-1-7-2019: Future propulsion and integration:... Specific Challenge:This action is part of the Aviation International Cooperation Flagship called "Sa...

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Este proyecto no cuenta con búsquedas de partenariado abiertas en este momento.

Información adicional privada

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36 Participantes

ONERA

1.77M€ | Lider

NIMGENETICS GENOMICA Y MEDIC...

255.50K€ | Participante

MTU

113.75K€ | Participante

SAFRAN ELECTRICAL POWER

71.03K€ | Participante

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Duración del proyecto: 54 meses Fecha Inicio: 2019-12-11
Fecha Fin: 2024-06-30

Líder del proyecto

OFFICE NATIONAL DETUDES ET DE RECHERCHES AERO... No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 19M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto To meet the goal of a carbon neutral growth of commercial aviation, the top level objective of IMOTHEP is to achieve a key step in assessing the potential offered by hybrid electric propulsion (HEP) and, ultimately, to build the corresponding aviation sector-wide roadmap for the maturation of the technology. The core of IMOTHEP is an integrated end-to-end investigation of hybrid-electric power trains for commercial aircraft, performed in close connexion with the propulsion system and aircraft architecture. Aircraft configurations will be selected based on their potential for fuel burn reduction and their representativeness of a variety of credible concepts, with a focus on regional and short-to-medium range missions. From the preliminary design of aircraft, target specifications will be defined for the architecture and components of the hybrid propulsion chain. Technological solutions and associated models will then be investigated with a twenty year timeframe perspective. In order to identify key technological enablers and technology gaps, the integrated performance of the electric components and power chain will be synthesized by assessing the fuel burn of the selected aircraft configurations, compared to conventional technologies extrapolated to 2035. The project will also address the infrastructures and tools required for HEP development, as well as the need for technology demonstrations or regulatory evolutions. Eventually, all these elements will feed the research and technology roadmap of HEP, which will constitute the final synthesis of the project. To achieve these ambitious goals, the 54-month project is supported by 7 R&D institutes, 11 industries (from aviation and electric systems), a service SME and 7 universities from 9 EU countries, plus 2 RTD organisations from Canada. The requested EU grant is 10 392 845 Euros.

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