Architecture of a remote impedance-based structural health monitoring system for aircraft applications

Detalhes bibliográficos
Autor(a) principal: Martins,Luiz G. A.
Data de Publicação: 2012
Outros Autores: Finzi Neto,Roberto M., Steffen Jr.,Valder, Palomino,Lizeth V., Rade,Domingos A.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782012000500008
Resumo: The essence of structural health monitoring (SHM) is to develop systems based on nondestructive inspection (NDI) technologies for continuous monitoring, inspection and detection of structural damages. A new architecture of a remote SHM system based on Electromechanical Impedance (EMI) measures is described in the present contribution. The proposed environment is employed to automatically monitor the structural integrity of aircrafts and is composed by sensor networks, a signal conditioning system, a data acquisition hardware and a data processing system. The obtained results allow the accomplishment of structural condition-based maintenance strategies, in opposite to those based only on the usage time of the equipment. This approach increases the operational capacity of the structure without compromising the security of the flights. As the environment continually checks for the first signs of damage, possibly reducing or eliminating scheduled aircraft inspections, it could significantly decrease maintenance and repair expenses. Furthermore, the usage of this system allows the creation of a historical database of the aircrafts structural integrity, making possible the incremental development of a Damage Prognosis System (DPS). This work presents the proposed architecture and a set of experiments that were conducted in a representative aircraft structure (aircraft window) to demonstrate the effectiveness of the proposed system.
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spelling Architecture of a remote impedance-based structural health monitoring system for aircraft applicationsStructural Health MonitoringNondestructive InspectionElectromechanical ImpedanceDamage PrognosisThe essence of structural health monitoring (SHM) is to develop systems based on nondestructive inspection (NDI) technologies for continuous monitoring, inspection and detection of structural damages. A new architecture of a remote SHM system based on Electromechanical Impedance (EMI) measures is described in the present contribution. The proposed environment is employed to automatically monitor the structural integrity of aircrafts and is composed by sensor networks, a signal conditioning system, a data acquisition hardware and a data processing system. The obtained results allow the accomplishment of structural condition-based maintenance strategies, in opposite to those based only on the usage time of the equipment. This approach increases the operational capacity of the structure without compromising the security of the flights. As the environment continually checks for the first signs of damage, possibly reducing or eliminating scheduled aircraft inspections, it could significantly decrease maintenance and repair expenses. Furthermore, the usage of this system allows the creation of a historical database of the aircrafts structural integrity, making possible the incremental development of a Damage Prognosis System (DPS). This work presents the proposed architecture and a set of experiments that were conducted in a representative aircraft structure (aircraft window) to demonstrate the effectiveness of the proposed system.Associação Brasileira de Engenharia e Ciências Mecânicas - ABCM2012-01-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782012000500008Journal of the Brazilian Society of Mechanical Sciences and Engineering v.34 n.spe 2012reponame:Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)instname:Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)instacron:ABCM10.1590/S1678-58782012000500008info:eu-repo/semantics/openAccessMartins,Luiz G. A.Finzi Neto,Roberto M.Steffen Jr.,ValderPalomino,Lizeth V.Rade,Domingos A.eng2013-01-28T00:00:00Zoai:scielo:S1678-58782012000500008Revistahttps://www.scielo.br/j/jbsmse/https://old.scielo.br/oai/scielo-oai.php||abcm@abcm.org.br1806-36911678-5878opendoar:2013-01-28T00:00Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online) - Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)false
dc.title.none.fl_str_mv Architecture of a remote impedance-based structural health monitoring system for aircraft applications
title Architecture of a remote impedance-based structural health monitoring system for aircraft applications
spellingShingle Architecture of a remote impedance-based structural health monitoring system for aircraft applications
Martins,Luiz G. A.
Structural Health Monitoring
Nondestructive Inspection
Electromechanical Impedance
Damage Prognosis
title_short Architecture of a remote impedance-based structural health monitoring system for aircraft applications
title_full Architecture of a remote impedance-based structural health monitoring system for aircraft applications
title_fullStr Architecture of a remote impedance-based structural health monitoring system for aircraft applications
title_full_unstemmed Architecture of a remote impedance-based structural health monitoring system for aircraft applications
title_sort Architecture of a remote impedance-based structural health monitoring system for aircraft applications
author Martins,Luiz G. A.
author_facet Martins,Luiz G. A.
Finzi Neto,Roberto M.
Steffen Jr.,Valder
Palomino,Lizeth V.
Rade,Domingos A.
author_role author
author2 Finzi Neto,Roberto M.
Steffen Jr.,Valder
Palomino,Lizeth V.
Rade,Domingos A.
author2_role author
author
author
author
dc.contributor.author.fl_str_mv Martins,Luiz G. A.
Finzi Neto,Roberto M.
Steffen Jr.,Valder
Palomino,Lizeth V.
Rade,Domingos A.
dc.subject.por.fl_str_mv Structural Health Monitoring
Nondestructive Inspection
Electromechanical Impedance
Damage Prognosis
topic Structural Health Monitoring
Nondestructive Inspection
Electromechanical Impedance
Damage Prognosis
description The essence of structural health monitoring (SHM) is to develop systems based on nondestructive inspection (NDI) technologies for continuous monitoring, inspection and detection of structural damages. A new architecture of a remote SHM system based on Electromechanical Impedance (EMI) measures is described in the present contribution. The proposed environment is employed to automatically monitor the structural integrity of aircrafts and is composed by sensor networks, a signal conditioning system, a data acquisition hardware and a data processing system. The obtained results allow the accomplishment of structural condition-based maintenance strategies, in opposite to those based only on the usage time of the equipment. This approach increases the operational capacity of the structure without compromising the security of the flights. As the environment continually checks for the first signs of damage, possibly reducing or eliminating scheduled aircraft inspections, it could significantly decrease maintenance and repair expenses. Furthermore, the usage of this system allows the creation of a historical database of the aircrafts structural integrity, making possible the incremental development of a Damage Prognosis System (DPS). This work presents the proposed architecture and a set of experiments that were conducted in a representative aircraft structure (aircraft window) to demonstrate the effectiveness of the proposed system.
publishDate 2012
dc.date.none.fl_str_mv 2012-01-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782012000500008
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782012000500008
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.1590/S1678-58782012000500008
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Associação Brasileira de Engenharia e Ciências Mecânicas - ABCM
publisher.none.fl_str_mv Associação Brasileira de Engenharia e Ciências Mecânicas - ABCM
dc.source.none.fl_str_mv Journal of the Brazilian Society of Mechanical Sciences and Engineering v.34 n.spe 2012
reponame:Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)
instname:Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron:ABCM
instname_str Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron_str ABCM
institution ABCM
reponame_str Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)
collection Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)
repository.name.fl_str_mv Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online) - Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
repository.mail.fl_str_mv ||abcm@abcm.org.br
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