Modeling and Sizing of a Fuel Cell—Lithium-Ion Battery Direct Hybridization System for Aeronautical Application

Nowadays, many aircraft manufacturers are working on new airplanes to reduce the environmental footprint and therefore meet greenhouse gas reduction targets. The concept of more electric aircraft is one of the solutions to achieve this goal. For this aircraft architecture, several electrical devices...

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Autores principales: Thomas Jarry, Fabien Lacressonnière, Amine Jaafar, Christophe Turpin, Marion Scohy
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Lenguaje:EN
Publicado: MDPI AG 2021
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spelling oai:doaj.org-article:80cffe89e5d44f3e9ad10020765647242021-11-25T17:27:34ZModeling and Sizing of a Fuel Cell—Lithium-Ion Battery Direct Hybridization System for Aeronautical Application10.3390/en142276551996-1073https://doaj.org/article/80cffe89e5d44f3e9ad10020765647242021-11-01T00:00:00Zhttps://www.mdpi.com/1996-1073/14/22/7655https://doaj.org/toc/1996-1073Nowadays, many aircraft manufacturers are working on new airplanes to reduce the environmental footprint and therefore meet greenhouse gas reduction targets. The concept of more electric aircraft is one of the solutions to achieve this goal. For this aircraft architecture, several electrical devices are used in order to supply propulsive and non-propulsive functions. This paper focuses on the sizing of a direct hybridization system to supply a non-propulsive function in an aircraft. It is composed of a High-Temperature Proton Exchange Membrane Fuel Cell (HT-PEMFC) and a lithium-ion (Li-ion) battery. This sizing is based on a static model of each storage device. The accuracy of these models is compared with dynamic models during a simulation for an aeronautical mission. Static models are implemented in a genetic algorithm to achieve two goals: on the one hand, satisfy the mission profile, and on the other hand, minimize the mass of the system. Other criteria, such as battery and fuel cell aging estimation, are considered. The obtained results show that the direct hybridization system allows protecting the fuel cell against an accelerated aging.Thomas JarryFabien LacressonnièreAmine JaafarChristophe TurpinMarion ScohyMDPI AGarticlehydrogenfuel cellshigh-temperature PEMFCbattery storagemore electric aircraftpassive hybridizationTechnologyTENEnergies, Vol 14, Iss 7655, p 7655 (2021)
institution DOAJ
collection DOAJ
language EN
topic hydrogen
fuel cells
high-temperature PEMFC
battery storage
more electric aircraft
passive hybridization
Technology
T
spellingShingle hydrogen
fuel cells
high-temperature PEMFC
battery storage
more electric aircraft
passive hybridization
Technology
T
Thomas Jarry
Fabien Lacressonnière
Amine Jaafar
Christophe Turpin
Marion Scohy
Modeling and Sizing of a Fuel Cell—Lithium-Ion Battery Direct Hybridization System for Aeronautical Application
description Nowadays, many aircraft manufacturers are working on new airplanes to reduce the environmental footprint and therefore meet greenhouse gas reduction targets. The concept of more electric aircraft is one of the solutions to achieve this goal. For this aircraft architecture, several electrical devices are used in order to supply propulsive and non-propulsive functions. This paper focuses on the sizing of a direct hybridization system to supply a non-propulsive function in an aircraft. It is composed of a High-Temperature Proton Exchange Membrane Fuel Cell (HT-PEMFC) and a lithium-ion (Li-ion) battery. This sizing is based on a static model of each storage device. The accuracy of these models is compared with dynamic models during a simulation for an aeronautical mission. Static models are implemented in a genetic algorithm to achieve two goals: on the one hand, satisfy the mission profile, and on the other hand, minimize the mass of the system. Other criteria, such as battery and fuel cell aging estimation, are considered. The obtained results show that the direct hybridization system allows protecting the fuel cell against an accelerated aging.
format article
author Thomas Jarry
Fabien Lacressonnière
Amine Jaafar
Christophe Turpin
Marion Scohy
author_facet Thomas Jarry
Fabien Lacressonnière
Amine Jaafar
Christophe Turpin
Marion Scohy
author_sort Thomas Jarry
title Modeling and Sizing of a Fuel Cell—Lithium-Ion Battery Direct Hybridization System for Aeronautical Application
title_short Modeling and Sizing of a Fuel Cell—Lithium-Ion Battery Direct Hybridization System for Aeronautical Application
title_full Modeling and Sizing of a Fuel Cell—Lithium-Ion Battery Direct Hybridization System for Aeronautical Application
title_fullStr Modeling and Sizing of a Fuel Cell—Lithium-Ion Battery Direct Hybridization System for Aeronautical Application
title_full_unstemmed Modeling and Sizing of a Fuel Cell—Lithium-Ion Battery Direct Hybridization System for Aeronautical Application
title_sort modeling and sizing of a fuel cell—lithium-ion battery direct hybridization system for aeronautical application
publisher MDPI AG
publishDate 2021
url https://doaj.org/article/80cffe89e5d44f3e9ad1002076564724
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AT aminejaafar modelingandsizingofafuelcelllithiumionbatterydirecthybridizationsystemforaeronauticalapplication
AT christopheturpin modelingandsizingofafuelcelllithiumionbatterydirecthybridizationsystemforaeronauticalapplication
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