Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application

Autores
Correa Perelmuter, Gabriel; Borello, Fabio; Santarelli, Massimo
Año de publicación
2015
Idioma
inglés
Tipo de recurso
artículo
Estado
versión publicada
Descripción
Experimental data concerning the reliability of fuel cell systems (FCS) in aviation are still unavailable to technical community, while assessing reliability of a component or a whole system represents a fundamental aspect that allows a new technology to be introduced in a high safety system such as an aircraft. The main aim of this paper is to show a method to estimate the reliability of an aircraft power system based on a hydrogen fuel cell, mainly for design purposes. The method is based on a high-order adaptive response surface technique, coupled with a dynamic model of the aircraft power system, and it is applied to the failure event represented by an incorrect power supply due to the failure of sensors of the control system of the powertrain. The most important advantage of the proposed method is the low computational effort it requires. The result is a ranking of the most critical sensors to be considered in the design phase of the power system and demonstrate that accurate temperature sensors and sensor calibration are of dramatic importance for the control of the stack power, in case of powertrain based on PEM fuel cell systems.
Fil: Correa Perelmuter, Gabriel. Universidad Nacional de Catamarca. Facultad de Ciencias Exactas y Naturales; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro de Investigaciones y Transferencia de Catamarca. Universidad Nacional de Catamarca. Centro de Investigaciones y Transferencia de Catamarca; Argentina
Fil: Borello, Fabio. Politecnico di Torino; Italia
Fil: Santarelli, Massimo. Politecnico di Torino; Italia
Materia
Pem Fuel Cell
Aircraft Uncertainty
Sensitivity
Dynamic Model
Nivel de accesibilidad
acceso abierto
Condiciones de uso
https://creativecommons.org/licenses/by-nc-sa/2.5/ar/
Repositorio
CONICET Digital (CONICET)
Institución
Consejo Nacional de Investigaciones Científicas y Técnicas
OAI Identificador
oai:ri.conicet.gov.ar:11336/41729
Acceder
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network_name_str CONICET Digital (CONICET)
spelling Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft applicationCorrea Perelmuter, GabrielBorello, FabioSantarelli, MassimoPem Fuel CellAircraft UncertaintySensitivityDynamic Modelhttps://purl.org/becyt/ford/2.2https://purl.org/becyt/ford/2Experimental data concerning the reliability of fuel cell systems (FCS) in aviation are still unavailable to technical community, while assessing reliability of a component or a whole system represents a fundamental aspect that allows a new technology to be introduced in a high safety system such as an aircraft. The main aim of this paper is to show a method to estimate the reliability of an aircraft power system based on a hydrogen fuel cell, mainly for design purposes. The method is based on a high-order adaptive response surface technique, coupled with a dynamic model of the aircraft power system, and it is applied to the failure event represented by an incorrect power supply due to the failure of sensors of the control system of the powertrain. The most important advantage of the proposed method is the low computational effort it requires. The result is a ranking of the most critical sensors to be considered in the design phase of the power system and demonstrate that accurate temperature sensors and sensor calibration are of dramatic importance for the control of the stack power, in case of powertrain based on PEM fuel cell systems.Fil: Correa Perelmuter, Gabriel. Universidad Nacional de Catamarca. Facultad de Ciencias Exactas y Naturales; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro de Investigaciones y Transferencia de Catamarca. Universidad Nacional de Catamarca. Centro de Investigaciones y Transferencia de Catamarca; ArgentinaFil: Borello, Fabio. Politecnico di Torino; ItaliaFil: Santarelli, Massimo. Politecnico di Torino; ItaliaPergamon-Elsevier Science Ltd2015-08info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionhttp://purl.org/coar/resource_type/c_6501info:ar-repo/semantics/articuloapplication/pdfapplication/pdfhttp://hdl.handle.net/11336/41729Correa Perelmuter, Gabriel; Borello, Fabio; Santarelli, Massimo; Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application; Pergamon-Elsevier Science Ltd; International Journal of Hydrogen Energy; 40; 8-2015; 10354-103650360-3199CONICET DigitalCONICETenginfo:eu-repo/semantics/altIdentifier/doi/10.1016/j.ijhydene.2015.05.133info:eu-repo/semantics/altIdentifier/url/https://www.sciencedirect.com/science/article/pii/S0360319915013464info:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by-nc-sa/2.5/ar/reponame:CONICET Digital (CONICET)instname:Consejo Nacional de Investigaciones Científicas y Técnicas2025-10-15T15:15:09Zoai:ri.conicet.gov.ar:11336/41729instacron:CONICETInstitucionalhttp://ri.conicet.gov.ar/Organismo científico-tecnológicoNo correspondehttp://ri.conicet.gov.ar/oai/requestdasensio@conicet.gov.ar; lcarlino@conicet.gov.arArgentinaNo correspondeNo correspondeNo correspondeopendoar:34982025-10-15 15:15:09.693CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicasfalse
dc.title.none.fl_str_mv Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
title Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
spellingShingle Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
Correa Perelmuter, Gabriel
Pem Fuel Cell
Aircraft Uncertainty
Sensitivity
Dynamic Model
title_short Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
title_full Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
title_fullStr Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
title_full_unstemmed Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
title_sort Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
dc.creator.none.fl_str_mv Correa Perelmuter, Gabriel
Borello, Fabio
Santarelli, Massimo
author Correa Perelmuter, Gabriel
author_facet Correa Perelmuter, Gabriel
Borello, Fabio
Santarelli, Massimo
author_role author
author2 Borello, Fabio
Santarelli, Massimo
author2_role author
author
dc.subject.none.fl_str_mv Pem Fuel Cell
Aircraft Uncertainty
Sensitivity
Dynamic Model
topic Pem Fuel Cell
Aircraft Uncertainty
Sensitivity
Dynamic Model
purl_subject.fl_str_mv https://purl.org/becyt/ford/2.2
https://purl.org/becyt/ford/2
dc.description.none.fl_txt_mv Experimental data concerning the reliability of fuel cell systems (FCS) in aviation are still unavailable to technical community, while assessing reliability of a component or a whole system represents a fundamental aspect that allows a new technology to be introduced in a high safety system such as an aircraft. The main aim of this paper is to show a method to estimate the reliability of an aircraft power system based on a hydrogen fuel cell, mainly for design purposes. The method is based on a high-order adaptive response surface technique, coupled with a dynamic model of the aircraft power system, and it is applied to the failure event represented by an incorrect power supply due to the failure of sensors of the control system of the powertrain. The most important advantage of the proposed method is the low computational effort it requires. The result is a ranking of the most critical sensors to be considered in the design phase of the power system and demonstrate that accurate temperature sensors and sensor calibration are of dramatic importance for the control of the stack power, in case of powertrain based on PEM fuel cell systems.
Fil: Correa Perelmuter, Gabriel. Universidad Nacional de Catamarca. Facultad de Ciencias Exactas y Naturales; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro de Investigaciones y Transferencia de Catamarca. Universidad Nacional de Catamarca. Centro de Investigaciones y Transferencia de Catamarca; Argentina
Fil: Borello, Fabio. Politecnico di Torino; Italia
Fil: Santarelli, Massimo. Politecnico di Torino; Italia
description Experimental data concerning the reliability of fuel cell systems (FCS) in aviation are still unavailable to technical community, while assessing reliability of a component or a whole system represents a fundamental aspect that allows a new technology to be introduced in a high safety system such as an aircraft. The main aim of this paper is to show a method to estimate the reliability of an aircraft power system based on a hydrogen fuel cell, mainly for design purposes. The method is based on a high-order adaptive response surface technique, coupled with a dynamic model of the aircraft power system, and it is applied to the failure event represented by an incorrect power supply due to the failure of sensors of the control system of the powertrain. The most important advantage of the proposed method is the low computational effort it requires. The result is a ranking of the most critical sensors to be considered in the design phase of the power system and demonstrate that accurate temperature sensors and sensor calibration are of dramatic importance for the control of the stack power, in case of powertrain based on PEM fuel cell systems.
publishDate 2015
dc.date.none.fl_str_mv 2015-08
dc.type.none.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
http://purl.org/coar/resource_type/c_6501
info:ar-repo/semantics/articulo
format article
status_str publishedVersion
dc.identifier.none.fl_str_mv http://hdl.handle.net/11336/41729
Correa Perelmuter, Gabriel; Borello, Fabio; Santarelli, Massimo; Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application; Pergamon-Elsevier Science Ltd; International Journal of Hydrogen Energy; 40; 8-2015; 10354-10365
0360-3199
CONICET Digital
CONICET
url http://hdl.handle.net/11336/41729
identifier_str_mv Correa Perelmuter, Gabriel; Borello, Fabio; Santarelli, Massimo; Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application; Pergamon-Elsevier Science Ltd; International Journal of Hydrogen Energy; 40; 8-2015; 10354-10365
0360-3199
CONICET Digital
CONICET
dc.language.none.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv info:eu-repo/semantics/altIdentifier/doi/10.1016/j.ijhydene.2015.05.133
info:eu-repo/semantics/altIdentifier/url/https://www.sciencedirect.com/science/article/pii/S0360319915013464
dc.rights.none.fl_str_mv info:eu-repo/semantics/openAccess
https://creativecommons.org/licenses/by-nc-sa/2.5/ar/
eu_rights_str_mv openAccess
rights_invalid_str_mv https://creativecommons.org/licenses/by-nc-sa/2.5/ar/
dc.format.none.fl_str_mv application/pdf
application/pdf
dc.publisher.none.fl_str_mv Pergamon-Elsevier Science Ltd
publisher.none.fl_str_mv Pergamon-Elsevier Science Ltd
dc.source.none.fl_str_mv reponame:CONICET Digital (CONICET)
instname:Consejo Nacional de Investigaciones Científicas y Técnicas
reponame_str CONICET Digital (CONICET)
collection CONICET Digital (CONICET)
instname_str Consejo Nacional de Investigaciones Científicas y Técnicas
repository.name.fl_str_mv CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicas
repository.mail.fl_str_mv dasensio@conicet.gov.ar; lcarlino@conicet.gov.ar
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score 13.22299

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