Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing

ilustraciones, diagramas

Autores:
León-Henao, Henry
Tipo de recurso:
Fecha de publicación:
2022
Institución:
Universidad Nacional de Colombia
Repositorio:
Universidad Nacional de Colombia
Idioma:
eng
OAI Identifier:
oai:repositorio.unal.edu.co:unal/82672
Acceso en línea:
https://repositorio.unal.edu.co/handle/unal/82672
https:/repositorio.una.edu.co
Palabra clave:
620 - Ingeniería y operaciones afines::629 - Otras ramas de la ingeniería
Levas
Turbinas de gas
Cams
Manufactura aditiva metales
Álabe GTD 111
L-PBF
L-DED
Additive Manufacturing
Gas turbine
Rights
openAccess
License
Reconocimiento 4.0 Internacional
id UNACIONAL2_9e503a96d949d1cb2fda011d13bf51b3
oai_identifier_str oai:repositorio.unal.edu.co:unal/82672
network_acronym_str UNACIONAL2
network_name_str Universidad Nacional de Colombia
repository_id_str
dc.title.eng.fl_str_mv Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing
dc.title.translated.spa.fl_str_mv Factibilidad técnica de la recuperación de álabes de GTD 111 degradados en servicio mediante tratamiento térmico y manufactura aditiva
title Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing
spellingShingle Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing
620 - Ingeniería y operaciones afines::629 - Otras ramas de la ingeniería
Levas
Turbinas de gas
Cams
Manufactura aditiva metales
Álabe GTD 111
L-PBF
L-DED
Additive Manufacturing
Gas turbine
title_short Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing
title_full Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing
title_fullStr Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing
title_full_unstemmed Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing
title_sort Technical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturing
dc.creator.fl_str_mv León-Henao, Henry
dc.contributor.advisor.none.fl_str_mv Toro Betancur, Alejandro
Giraldo Barrada, Jorge Enrique
dc.contributor.author.none.fl_str_mv León-Henao, Henry
dc.contributor.researchgroup.spa.fl_str_mv Grupo de Soldadura
Grupo de Investigación en Corrosión, Tribologia y Energía
dc.contributor.orcid.spa.fl_str_mv León Henao, Henry [0000-0002-1582-9386]
Giraldo Barrada, Jorge Enrique [0000-0001-6614-0661]
dc.contributor.googlescholar.spa.fl_str_mv Henry León-Henao
dc.subject.ddc.spa.fl_str_mv 620 - Ingeniería y operaciones afines::629 - Otras ramas de la ingeniería
topic 620 - Ingeniería y operaciones afines::629 - Otras ramas de la ingeniería
Levas
Turbinas de gas
Cams
Manufactura aditiva metales
Álabe GTD 111
L-PBF
L-DED
Additive Manufacturing
Gas turbine
dc.subject.lemb.spa.fl_str_mv Levas
Turbinas de gas
dc.subject.lemb.eng.fl_str_mv Cams
dc.subject.proposal.spa.fl_str_mv Manufactura aditiva metales
Álabe GTD 111
dc.subject.proposal.eng.fl_str_mv L-PBF
L-DED
Additive Manufacturing
Gas turbine
description ilustraciones, diagramas
publishDate 2022
dc.date.accessioned.none.fl_str_mv 2022-11-09T17:04:23Z
dc.date.available.none.fl_str_mv 2022-11-09T17:04:23Z
dc.date.issued.none.fl_str_mv 2022-08-08
dc.type.spa.fl_str_mv Trabajo de grado - Maestría
dc.type.driver.spa.fl_str_mv info:eu-repo/semantics/masterThesis
dc.type.version.spa.fl_str_mv info:eu-repo/semantics/acceptedVersion
dc.type.content.spa.fl_str_mv Text
dc.type.redcol.spa.fl_str_mv http://purl.org/redcol/resource_type/TM
status_str acceptedVersion
dc.identifier.uri.none.fl_str_mv https://repositorio.unal.edu.co/handle/unal/82672
dc.identifier.instname.spa.fl_str_mv Universidad Nacional de Colombia
dc.identifier.reponame.spa.fl_str_mv Repositorio Institucional Universidad Nacional de Colombia
dc.identifier.repourl.spa.fl_str_mv https:/repositorio.una.edu.co
url https://repositorio.unal.edu.co/handle/unal/82672
https:/repositorio.una.edu.co
identifier_str_mv Universidad Nacional de Colombia
Repositorio Institucional Universidad Nacional de Colombia
dc.language.iso.spa.fl_str_mv eng
language eng
dc.relation.indexed.spa.fl_str_mv RedCol
LaReferencia
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dc.rights.license.spa.fl_str_mv Reconocimiento 4.0 Internacional
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dc.format.extent.spa.fl_str_mv 152 páginas
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dc.publisher.spa.fl_str_mv Universidad Nacional de Colombia
dc.publisher.program.spa.fl_str_mv Medellín - Minas - Maestría en Ingeniería Mecánica
dc.publisher.faculty.spa.fl_str_mv Facultad de Minas
dc.publisher.place.spa.fl_str_mv Medellín, Colombia
dc.publisher.branch.spa.fl_str_mv Universidad Nacional de Colombia - Sede Medellín
institution Universidad Nacional de Colombia
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spelling Reconocimiento 4.0 Internacionalhttp://creativecommons.org/licenses/by/4.0/info:eu-repo/semantics/openAccesshttp://purl.org/coar/access_right/c_abf2Toro Betancur, Alejandroeef8cfc23e5965d8d651306ca5a5e8c7Giraldo Barrada, Jorge Enrique02940d1aa0f9f6e96d7caa3ef6691328600León-Henao, Henryd50aae118a882cb0a32fff658fe3fff9600Grupo de SoldaduraGrupo de Investigación en Corrosión, Tribologia y EnergíaLeón Henao, Henry [0000-0002-1582-9386]Giraldo Barrada, Jorge Enrique [0000-0001-6614-0661]Henry León-Henao2022-11-09T17:04:23Z2022-11-09T17:04:23Z2022-08-08https://repositorio.unal.edu.co/handle/unal/82672Universidad Nacional de ColombiaRepositorio Institucional Universidad Nacional de Colombiahttps:/repositorio.una.edu.coilustraciones, diagramasRepair components of the hot gas path is crucial for economic reasons in gas turbine engines. In this work, a characterization of deposits applied by Laser Powder Bed Fusion (LPBF) and Laser Powder Directed Energized Deposition (LP-DED) on a 1st stage blade made of GTD 111 DS superalloy were carried out. The 1st stage blades are damaged in operation due to collision of external objects, development of thermal fatigue cracks and hightemperature erosion, which drastically reduces their lifetime. The process parameters for LDED and L-PBF were established as a function of the integrity and geometry of the deposits. René 65 powder was used for both processes without preheating. Visual inspection and macro etching were used to evaluate the weld metal deposits soundness. Optical microscopy and scanning electron microscopy were used to examine the microstructure of the deposited layers in the cross-section and EBSD allowed studying the crystallographic texture. Compared to conventional processes, L-PBF and LP-DED provide crack-free deposits and better control of shape and dimensions, reducing machining time. In particular, the L-PBF process has greater precision, which makes it ideal for replicating the blade’s cooling holes. The study demonstrates the feasibility to restore dimensions of a tip blades and illustrates the significant potential of Additive Manufacturing (AM) utilizing powders of high γ' avoiding hot cracking.La reparación de los componentes de la ruta del gas caliente es crucial por razones económicas en las turbinas a gas. En este trabajo se realizó una caracterización de los depósitos aplicados por Laser Powder Bed Fusion (L-PBF) y Laser Powder Directed Energized Deposition (LP-DED) sobre un álabe de primera etapa fabricado con la superaleación GTD 111 DS. Al deteriorarse en funcionamiento debido a la colisión de objetos externos, el crecimiento de grietas por fatiga térmica y la erosión por alta temperatura, se reduce drásticamente su vida útil. Los parámetros del proceso para L-DED y L-PBF se establecieron en función de la integridad y la geometría de los depósitos. Para ambos procesos se utilizó polvo René 65 sin precalentamiento. Se utilizó inspección visual y análisis metalográfico para evaluar la solidez de los depósitos de manufactura aditiva. Se usó microscopía óptica y microscopía electrónica de barrido para examinar la microestructura de las capas depositadas en la sección transversal y el análisis de EBSD permitió estudiar la textura cristalográfica. En comparación con los procesos convencionales, L-PBF y LP-DED proporcionan depósitos sin grietas y un mejor control de la forma y las dimensiones, lo que reduce el tiempo de mecanizado. En particular, el proceso L-PBF tiene una mayor precisión, lo que lo hace ideal para replicar los orificios de enfriamiento de la hoja. El estudio demuestra la viabilidad de restaurar las dimensiones de los álabes en el borde chirriante e ilustra el importante potencial de la fabricación aditiva (FA) que utiliza polvos de alto contenido de γ' evitando el agrietamiento en caliente. (Texto tomado de la fuente)MaestríaMagíster en Ingeniería MecánicaSoldadura. Manufactura aditivaÁrea Curricular de Ingeniería Mecánica152 páginasapplication/pdfengUniversidad Nacional de ColombiaMedellín - Minas - Maestría en Ingeniería MecánicaFacultad de MinasMedellín, ColombiaUniversidad Nacional de Colombia - Sede Medellín620 - Ingeniería y operaciones afines::629 - Otras ramas de la ingenieríaLevasTurbinas de gasCamsManufactura aditiva metalesÁlabe GTD 111L-PBFL-DEDAdditive ManufacturingGas turbineTechnical feasibility of recovering degraded GTD 111 blades in service through heat treatment and additive manufacturingFactibilidad técnica de la recuperación de álabes de GTD 111 degradados en servicio mediante tratamiento térmico y manufactura aditivaTrabajo de grado - Maestríainfo:eu-repo/semantics/masterThesisinfo:eu-repo/semantics/acceptedVersionTexthttp://purl.org/redcol/resource_type/TMRedColLaReferenciaA. Lou, C. Grosvenor, Selective laser sintering, birth of an industry, http://www.me.utexas.edu/news/news/selective-laser-sintering-birth-of-an-industry. 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Materials & Design, 197, 109214.InvestigadoresLICENSElicense.txtlicense.txttext/plain; charset=utf-85879https://repositorio.unal.edu.co/bitstream/unal/82672/1/license.txteb34b1cf90b7e1103fc9dfd26be24b4aMD51ORIGINALTesis de Maestría en Ingeniería Mecánica_Henry Leon Henao 1088291511.2022.pdfTesis de Maestría en Ingeniería Mecánica_Henry Leon Henao 1088291511.2022.pdfTesis de Maestría en Ingeniería Mecánicaapplication/pdf14845936https://repositorio.unal.edu.co/bitstream/unal/82672/2/Tesis%20de%20Maestr%c3%ada%20en%20Ingenier%c3%ada%20Mec%c3%a1nica_Henry%20Leon%20Henao%201088291511.2022.pdfeb7a47ff9a08a1b3883406c2e9e4ade4MD52unal/82672oai:repositorio.unal.edu.co:unal/826722022-11-09 12:10:18.517Repositorio Institucional Universidad Nacional de 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