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Next generation of improved High Temperature Membrane Electrode Assembly for Aviation

Descrizione del progetto

L’aviazione fa rotta verso le celle a combustibile a idrogeno

I sistemi a celle a combustibile (FC, Fuel Cell) a idrogeno, che rappresentano un’alternativa più pulita per l’aviazione, possono offrire un’elevata efficienza energetica e portare a una riduzione delle emissioni acustiche. In proposito, il progetto NIMPHEA, finanziato dall’UE, svilupperà una nuova generazione di assemblati membrana-elettrodi (MEA, Membrane Electrode Assembly) ad alta temperatura per FC a idrogeno in grado di alimentare gli aerei senza emettere sostanze inquinanti. Sebbene i MEA a bassa temperatura abbiano un’interessante densità di potenza, le criticità per quanto riguarda la gestione termica li rendono incompatibili con gli ambienti degli aerei. D’altra parte, anche gli attuali FC ad alta temperatura, che funzionano a circa 160 °C, non soddisfano i requisiti di prestazione per le applicazioni aeronautiche. Il progetto NIMPHEA mira quindi a ottimizzare i componenti principali dei MEA (strato catalizzatore, membrana e strato di diffusione del gas) per raggiungere una densità di potenza di 1,25 W/cm² a una temperatura di esercizio nominale di 120 °C.

Obiettivo

H2-based fuel cell systems (FCs) are a promising solution to power aircrafts without emitting CO2 or NOx and thus have the potential to strongly reduce aviation emissions and pave the way to climate neutrality. Embedded in aircrafts, FCs can supply non-propulsive and propulsive energy without pollutant emission, reduced noise emission and attractive energy efficiency.
The Low Temperature Proton Exchange Membrane (LT-PEM) technology (incl. Membrane Electrode Assembly - MEA) emerging from the automotive industry is of great interest for aviation, but thermal management issues are still be solved. Operated below 100°C, they exhibit attractive power density but are incompatible with aircraft environment due to poor heat rejection. Also, current High Temperature FCs operated around 160°C are not at the expected level of performance for aviation, despite interesting heat rejection performances. The development of a new-generation MEA, working at temperature above 120°C and with performances equivalent to current LT-PEM MEA is the key to unlock FC applications for aviation.
NIMPHEA aims at developing - based on the development and/or optimisation of its components: catalyst layer, membrane and gas diffusion layer - a new-generation HT MEA compatible with aircraft environment and requirements, considering a system size of 1.5 MW and contributing to higher level FC targets: a power density of 1.25 W/cm² at nominal operating temperature comprised between 160°C-200°C. MEA components’ upscale synthesis and assembly process will be assessed by identifying process parameters and improved through an iterative process with lab-scale MEA tests. This disruptive MEA technology will be finally validated in a representative scale prototype (165-180 cm²) embodied in a single-cell. Simultaneously, LCA, LCC, eco-efficiency assessment and intrinsic hazard analysis will be performed to validate the MEA development. Finally, a TRL evaluation will be conducted to validate TRL4.

Coordinatore

SAFRAN POWER UNITS
Contribution nette de l'UE
€ 1 483 980,00
Indirizzo
8 CHEMIN DU PONT DE RUPE
31200 Toulouse
Francia

Mostra sulla mappa

Regione
Occitanie Midi-Pyrénées Haute-Garonne
Tipo di attività
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Collegamenti
Costo totale
€ 1 483 980,00

Partecipanti (7)