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dc.rights.licenseAtribución-NoComercial 4.0 Internacional
dc.contributor.authorOsorio Ramírez, Julián David
dc.contributor.authorToro Betancur, Alejandro Octavio
dc.contributor.authorHernández Ortiz, Juan Pablo
dc.date.accessioned2019-06-28T04:08:22Z
dc.date.available2019-06-28T04:08:22Z
dc.date.issued2012
dc.identifier.urihttps://repositorio.unal.edu.co/handle/unal/39604
dc.description.abstractAdvances in new materials for current power generation devices, such as gas turbines, have led to more efficient and durable engines that supply rising energy demands. High efficiencies in gas turbines, due to higher operating temperatures, have been accomplished through the development of thermal barrier coatings. These are multilayered systems that provide thermal isolation capability and protection against corrosion and high temperature erosion. In this work, we describe the barrier’s application processes, their microstructural characteristics and their main failure mechanisms. Two different thermal barrier coatings are characterized and the most relevant trends of these systems are summarized.
dc.format.mimetypeapplication/pdf
dc.language.isospa
dc.publisherUniversidad Nacional de Colombia Sede Medellín
dc.relationhttp://revistas.unal.edu.co/index.php/dyna/article/view/28328
dc.relation.ispartofUniversidad Nacional de Colombia Revistas electrónicas UN Dyna
dc.relation.ispartofDyna
dc.relation.ispartofseriesDyna; Vol. 79, núm. 176 (2012); 149-158 DYNA; Vol. 79, núm. 176 (2012); 149-158 2346-2183 0012-7353
dc.rightsDerechos reservados - Universidad Nacional de Colombia
dc.rights.urihttp://creativecommons.org/licenses/by-nc/4.0/
dc.titleThermal barrier coatings for gas turbine applications: failure mechanisms and key microstructural features
dc.typeArtículo de revista
dc.type.driverinfo:eu-repo/semantics/article
dc.type.versioninfo:eu-repo/semantics/publishedVersion
dc.identifier.eprintshttp://bdigital.unal.edu.co/29701/
dc.relation.referencesOsorio Ramírez, Julián David and Toro Betancur, Alejandro Octavio and Hernández Ortiz, Juan Pablo (2012) Thermal barrier coatings for gas turbine applications: failure mechanisms and key microstructural features. Dyna; Vol. 79, núm. 176 (2012); 149-158 DYNA; Vol. 79, núm. 176 (2012); 149-158 2346-2183 0012-7353 .
dc.rights.accessrightsinfo:eu-repo/semantics/openAccess
dc.subject.proposalThermal Barrier Coating (TBC)
dc.subject.proposalGas Turbine
dc.subject.proposalFailure mechanisms
dc.type.coarhttp://purl.org/coar/resource_type/c_6501
dc.type.coarversionhttp://purl.org/coar/version/c_970fb48d4fbd8a85
dc.type.contentText
dc.type.redcolhttp://purl.org/redcol/resource_type/ART
oaire.accessrightshttp://purl.org/coar/access_right/c_abf2


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Atribución-NoComercial 4.0 InternacionalEsta obra está bajo licencia internacional Creative Commons Reconocimiento-NoComercial 4.0.Este documento ha sido depositado por parte de el(los) autor(es) bajo la siguiente constancia de depósito