Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft

Autores
Correa Perelmuter, Gabriel; Santarelli, Massimo; Borello, F.; Cestino, E.; Romeo, G.
Año de publicación
2015
Idioma
inglés
Tipo de recurso
artículo
Estado
versión publicada
Descripción
The application of fuel cell technology to aircraft propulsion and/or energy supply is attracting a great deal of interest because of the undoubted advantages that can be attained in terms of pollution emissions and noise reduction. The goal of the ENFICA-FC project (Environmentally Friendly Inter City Aircraft powered by Fuel Cells) has been to develop and validate new fuel cell-based power system concepts for more/all electric aircrafts pertaining to the "inter-city" segment of the market. As a result of the project, a technology demonstrator has been designed, manufactured, and tested: a proton exchange membrane (PEM) fuel cell-based power system was installed in the Skyleader RAPID200 aircraft which underwent its demonstrative flights in 2010. On the basis of the flight experiences gained during the ENFICA-FC program, the main topic of this paper is the description and validation of the multi-disciplinary dynamic model of the PEMFC-based powertrain of the ultra-light aircraft, fed with a pure hydrogen flow. Within this paper, emphasis is given to the model validation and dynamic system behavior. In order to validate the predicted results, data from real fuel cell flight (two 40-minute missions performed during the ENFICA-FC test campaign) have been used and are presented in this paper.
Fil: Correa Perelmuter, Gabriel. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina. Universidad Nacional de Catamarca. Facultad de Ciencias Exactas y Naturales; Argentina
Fil: Santarelli, Massimo. Politecnico di Torino; Italia
Fil: Borello, F.. Politecnico di Torino; Italia
Fil: Cestino, E.. Politecnico di Torino; Italia
Fil: Romeo, G.. Politecnico di Torino; Italia
Materia
Balance of Plant Model
Dynamic Model
Flight Test Experimental Validation
Fuel Cell Aircraft
Pem Hydrogen Fuel Cell
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:11336/38586
Acceder
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oai_identifier_str oai:ri.conicet.gov.ar:11336/38586
network_acronym_str CONICETDig
repository_id_str 3498
network_name_str CONICET Digital (CONICET)
spelling Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraftCorrea Perelmuter, GabrielSantarelli, MassimoBorello, F.Cestino, E.Romeo, G.Balance of Plant ModelDynamic ModelFlight Test Experimental ValidationFuel Cell AircraftPem Hydrogen Fuel Cellhttps://purl.org/becyt/ford/2.3https://purl.org/becyt/ford/2The application of fuel cell technology to aircraft propulsion and/or energy supply is attracting a great deal of interest because of the undoubted advantages that can be attained in terms of pollution emissions and noise reduction. The goal of the ENFICA-FC project (Environmentally Friendly Inter City Aircraft powered by Fuel Cells) has been to develop and validate new fuel cell-based power system concepts for more/all electric aircrafts pertaining to the "inter-city" segment of the market. As a result of the project, a technology demonstrator has been designed, manufactured, and tested: a proton exchange membrane (PEM) fuel cell-based power system was installed in the Skyleader RAPID200 aircraft which underwent its demonstrative flights in 2010. On the basis of the flight experiences gained during the ENFICA-FC program, the main topic of this paper is the description and validation of the multi-disciplinary dynamic model of the PEMFC-based powertrain of the ultra-light aircraft, fed with a pure hydrogen flow. Within this paper, emphasis is given to the model validation and dynamic system behavior. In order to validate the predicted results, data from real fuel cell flight (two 40-minute missions performed during the ENFICA-FC test campaign) have been used and are presented in this paper.Fil: Correa Perelmuter, Gabriel. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina. Universidad Nacional de Catamarca. Facultad de Ciencias Exactas y Naturales; ArgentinaFil: Santarelli, Massimo. Politecnico di Torino; ItaliaFil: Borello, F.. Politecnico di Torino; ItaliaFil: Cestino, E.. Politecnico di Torino; ItaliaFil: Romeo, G.. Politecnico di Torino; ItaliaProfessional Engineering Publishing Ltd2015-04info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionhttp://purl.org/coar/resource_type/c_6501info:ar-repo/semantics/articuloapplication/pdfapplication/pdfhttp://hdl.handle.net/11336/38586Correa Perelmuter, Gabriel; Santarelli, Massimo; Borello, F.; Cestino, E.; Romeo, G.; Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft; Professional Engineering Publishing Ltd; Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering; 229; 5; 4-2015; 917-9320954-4100CONICET DigitalCONICETenginfo:eu-repo/semantics/altIdentifier/doi/10.1177/0954410014541081info:eu-repo/semantics/altIdentifier/url/http://journals.sagepub.com/doi/abs/10.1177/0954410014541081info:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by-nc-sa/2.5/ar/reponame:CONICET Digital (CONICET)instname:Consejo Nacional de Investigaciones Científicas y Técnicas2025-10-15T15:43:37Zoai:ri.conicet.gov.ar:11336/38586instacron: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 15:43:38.143CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicasfalse
dc.title.none.fl_str_mv Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
title Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
spellingShingle Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
Correa Perelmuter, Gabriel
Balance of Plant Model
Dynamic Model
Flight Test Experimental Validation
Fuel Cell Aircraft
Pem Hydrogen Fuel Cell
title_short Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
title_full Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
title_fullStr Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
title_full_unstemmed Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
title_sort Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
dc.creator.none.fl_str_mv Correa Perelmuter, Gabriel
Santarelli, Massimo
Borello, F.
Cestino, E.
Romeo, G.
author Correa Perelmuter, Gabriel
author_facet Correa Perelmuter, Gabriel
Santarelli, Massimo
Borello, F.
Cestino, E.
Romeo, G.
author_role author
author2 Santarelli, Massimo
Borello, F.
Cestino, E.
Romeo, G.
author2_role author
author
author
author
dc.subject.none.fl_str_mv Balance of Plant Model
Dynamic Model
Flight Test Experimental Validation
Fuel Cell Aircraft
Pem Hydrogen Fuel Cell
topic Balance of Plant Model
Dynamic Model
Flight Test Experimental Validation
Fuel Cell Aircraft
Pem Hydrogen Fuel Cell
purl_subject.fl_str_mv https://purl.org/becyt/ford/2.3
https://purl.org/becyt/ford/2
dc.description.none.fl_txt_mv The application of fuel cell technology to aircraft propulsion and/or energy supply is attracting a great deal of interest because of the undoubted advantages that can be attained in terms of pollution emissions and noise reduction. The goal of the ENFICA-FC project (Environmentally Friendly Inter City Aircraft powered by Fuel Cells) has been to develop and validate new fuel cell-based power system concepts for more/all electric aircrafts pertaining to the "inter-city" segment of the market. As a result of the project, a technology demonstrator has been designed, manufactured, and tested: a proton exchange membrane (PEM) fuel cell-based power system was installed in the Skyleader RAPID200 aircraft which underwent its demonstrative flights in 2010. On the basis of the flight experiences gained during the ENFICA-FC program, the main topic of this paper is the description and validation of the multi-disciplinary dynamic model of the PEMFC-based powertrain of the ultra-light aircraft, fed with a pure hydrogen flow. Within this paper, emphasis is given to the model validation and dynamic system behavior. In order to validate the predicted results, data from real fuel cell flight (two 40-minute missions performed during the ENFICA-FC test campaign) have been used and are presented in this paper.
Fil: Correa Perelmuter, Gabriel. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina. Universidad Nacional de Catamarca. Facultad de Ciencias Exactas y Naturales; Argentina
Fil: Santarelli, Massimo. Politecnico di Torino; Italia
Fil: Borello, F.. Politecnico di Torino; Italia
Fil: Cestino, E.. Politecnico di Torino; Italia
Fil: Romeo, G.. Politecnico di Torino; Italia
description The application of fuel cell technology to aircraft propulsion and/or energy supply is attracting a great deal of interest because of the undoubted advantages that can be attained in terms of pollution emissions and noise reduction. The goal of the ENFICA-FC project (Environmentally Friendly Inter City Aircraft powered by Fuel Cells) has been to develop and validate new fuel cell-based power system concepts for more/all electric aircrafts pertaining to the "inter-city" segment of the market. As a result of the project, a technology demonstrator has been designed, manufactured, and tested: a proton exchange membrane (PEM) fuel cell-based power system was installed in the Skyleader RAPID200 aircraft which underwent its demonstrative flights in 2010. On the basis of the flight experiences gained during the ENFICA-FC program, the main topic of this paper is the description and validation of the multi-disciplinary dynamic model of the PEMFC-based powertrain of the ultra-light aircraft, fed with a pure hydrogen flow. Within this paper, emphasis is given to the model validation and dynamic system behavior. In order to validate the predicted results, data from real fuel cell flight (two 40-minute missions performed during the ENFICA-FC test campaign) have been used and are presented in this paper.
publishDate 2015
dc.date.none.fl_str_mv 2015-04
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/11336/38586
Correa Perelmuter, Gabriel; Santarelli, Massimo; Borello, F.; Cestino, E.; Romeo, G.; Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft; Professional Engineering Publishing Ltd; Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering; 229; 5; 4-2015; 917-932
0954-4100
CONICET Digital
CONICET
url http://hdl.handle.net/11336/38586
identifier_str_mv Correa Perelmuter, Gabriel; Santarelli, Massimo; Borello, F.; Cestino, E.; Romeo, G.; Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft; Professional Engineering Publishing Ltd; Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering; 229; 5; 4-2015; 917-932
0954-4100
CONICET Digital
CONICET
dc.language.none.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv info:eu-repo/semantics/altIdentifier/doi/10.1177/0954410014541081
info:eu-repo/semantics/altIdentifier/url/http://journals.sagepub.com/doi/abs/10.1177/0954410014541081
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 Professional Engineering Publishing Ltd
publisher.none.fl_str_mv Professional Engineering Publishing 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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