Probabilistic damage tolerance analysis using inspection data from integrated sensors
ABSTRACT : Fatigue failures are common failures within the aeronautical field. microcracks appear after many repetitions of cyclic stresses, then, these microcracks grow until a point of no return is reached and the growth becomes unstable and imminent. It is hard to do reliable estimations of a sys...
- Autores:
-
Vallejo Ciro, María Isabel
Carvajal Loaiza, Manuel José
- Tipo de recurso:
- Trabajo de grado de pregrado
- Fecha de publicación:
- 2021
- Institución:
- Universidad de Antioquia
- Repositorio:
- Repositorio UdeA
- Idioma:
- eng
- OAI Identifier:
- oai:bibliotecadigital.udea.edu.co:10495/25415
- Acceso en línea:
- http://hdl.handle.net/10495/25415
- Palabra clave:
- Aeronautics - Safety measures
Aeronáutica - medidas de seguridad
Fracture of solids
Fractura de sólidos
Fracture strength
Resistencia a las fracturas
Materials fatigue
Fatiga de materiales
Probabilities
Probabilidades
Residual stresse
Esfuerzos residuales
Stability of airplanes
Estabilidad de los aviones
Sensors
Sensores
Bayesian updating
http://aims.fao.org/aos/agrovoc/c_28279
- Rights
- openAccess
- License
- http://creativecommons.org/licenses/by-nc-sa/2.5/co/
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UDEA2 |
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Repositorio UdeA |
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|
dc.title.spa.fl_str_mv |
Probabilistic damage tolerance analysis using inspection data from integrated sensors |
title |
Probabilistic damage tolerance analysis using inspection data from integrated sensors |
spellingShingle |
Probabilistic damage tolerance analysis using inspection data from integrated sensors Aeronautics - Safety measures Aeronáutica - medidas de seguridad Fracture of solids Fractura de sólidos Fracture strength Resistencia a las fracturas Materials fatigue Fatiga de materiales Probabilities Probabilidades Residual stresse Esfuerzos residuales Stability of airplanes Estabilidad de los aviones Sensors Sensores Bayesian updating http://aims.fao.org/aos/agrovoc/c_28279 |
title_short |
Probabilistic damage tolerance analysis using inspection data from integrated sensors |
title_full |
Probabilistic damage tolerance analysis using inspection data from integrated sensors |
title_fullStr |
Probabilistic damage tolerance analysis using inspection data from integrated sensors |
title_full_unstemmed |
Probabilistic damage tolerance analysis using inspection data from integrated sensors |
title_sort |
Probabilistic damage tolerance analysis using inspection data from integrated sensors |
dc.creator.fl_str_mv |
Vallejo Ciro, María Isabel Carvajal Loaiza, Manuel José |
dc.contributor.advisor.none.fl_str_mv |
Ocampo de los Ríos, Juan David Bustamante Góez, Liliana Marcela |
dc.contributor.author.none.fl_str_mv |
Vallejo Ciro, María Isabel Carvajal Loaiza, Manuel José |
dc.subject.lemb.none.fl_str_mv |
Aeronautics - Safety measures Aeronáutica - medidas de seguridad Fracture of solids Fractura de sólidos Fracture strength Resistencia a las fracturas Materials fatigue Fatiga de materiales Probabilities Probabilidades Residual stresse Esfuerzos residuales Stability of airplanes Estabilidad de los aviones |
topic |
Aeronautics - Safety measures Aeronáutica - medidas de seguridad Fracture of solids Fractura de sólidos Fracture strength Resistencia a las fracturas Materials fatigue Fatiga de materiales Probabilities Probabilidades Residual stresse Esfuerzos residuales Stability of airplanes Estabilidad de los aviones Sensors Sensores Bayesian updating http://aims.fao.org/aos/agrovoc/c_28279 |
dc.subject.agrovoc.none.fl_str_mv |
Sensors Sensores |
dc.subject.proposal.spa.fl_str_mv |
Bayesian updating |
dc.subject.agrovocuri.none.fl_str_mv |
http://aims.fao.org/aos/agrovoc/c_28279 |
description |
ABSTRACT : Fatigue failures are common failures within the aeronautical field. microcracks appear after many repetitions of cyclic stresses, then, these microcracks grow until a point of no return is reached and the growth becomes unstable and imminent. It is hard to do reliable estimations of a system subject to fatigue due to multiple random factors that affect the material, geometry, and stresses, among others. In this work, to estimate this type of failure, a probabilistic analysis is performed, where each parameter from the model is represented as a probability density function. This work presents a software application to perform fatigue failure analysis using MATLAB and SMART|DT. This last program follows the standards issued by the Federal Aviation Administration of United States (FAA). The application implements a Bayesian inference process to update the model’s crack size distribution when inspections are performed, to add more accuracy to risk predictions. This application is expected to support decisions about when to perform inspections based on an allowable desired risk for the fleet. |
publishDate |
2021 |
dc.date.issued.none.fl_str_mv |
2021 |
dc.date.accessioned.none.fl_str_mv |
2022-01-19T21:23:19Z |
dc.date.available.none.fl_str_mv |
2022-01-19T21:23:19Z |
dc.type.spa.fl_str_mv |
info:eu-repo/semantics/bachelorThesis |
dc.type.coarversion.fl_str_mv |
http://purl.org/coar/version/c_b1a7d7d4d402bcce |
dc.type.hasversion.spa.fl_str_mv |
info:eu-repo/semantics/draft |
dc.type.coar.spa.fl_str_mv |
http://purl.org/coar/resource_type/c_7a1f |
dc.type.redcol.spa.fl_str_mv |
https://purl.org/redcol/resource_type/TP |
dc.type.local.spa.fl_str_mv |
Tesis/Trabajo de grado - Monografía - Pregrado |
format |
http://purl.org/coar/resource_type/c_7a1f |
status_str |
draft |
dc.identifier.uri.none.fl_str_mv |
http://hdl.handle.net/10495/25415 |
url |
http://hdl.handle.net/10495/25415 |
dc.language.iso.spa.fl_str_mv |
eng |
language |
eng |
dc.rights.spa.fl_str_mv |
info:eu-repo/semantics/openAccess |
dc.rights.uri.*.fl_str_mv |
http://creativecommons.org/licenses/by-nc-sa/2.5/co/ |
dc.rights.accessrights.spa.fl_str_mv |
http://purl.org/coar/access_right/c_abf2 |
dc.rights.creativecommons.spa.fl_str_mv |
https://creativecommons.org/licenses/by-nc-sa/4.0/ |
eu_rights_str_mv |
openAccess |
rights_invalid_str_mv |
http://creativecommons.org/licenses/by-nc-sa/2.5/co/ http://purl.org/coar/access_right/c_abf2 https://creativecommons.org/licenses/by-nc-sa/4.0/ |
dc.format.extent.spa.fl_str_mv |
67 |
dc.format.mimetype.spa.fl_str_mv |
application/pdf |
dc.publisher.group.spa.fl_str_mv |
Grupo de Diseño Mecánico |
dc.publisher.place.spa.fl_str_mv |
Medellín |
institution |
Universidad de Antioquia |
bitstream.url.fl_str_mv |
https://bibliotecadigital.udea.edu.co/bitstream/10495/25415/4/license.txt https://bibliotecadigital.udea.edu.co/bitstream/10495/25415/3/license_rdf https://bibliotecadigital.udea.edu.co/bitstream/10495/25415/1/VallejoMaria_2021_DamageToleranceAnalysis.pdf https://bibliotecadigital.udea.edu.co/bitstream/10495/25415/2/AutorizacionDePublicacion.pdf |
bitstream.checksum.fl_str_mv |
8a4605be74aa9ea9d79846c1fba20a33 e2060682c9c70d4d30c83c51448f4eed 4f5eb882b663070e648365c53bc92f72 9d398dd594616d24dc56cde0a69a7e81 |
bitstream.checksumAlgorithm.fl_str_mv |
MD5 MD5 MD5 MD5 |
repository.name.fl_str_mv |
Repositorio Institucional Universidad de Antioquia |
repository.mail.fl_str_mv |
andres.perez@udea.edu.co |
_version_ |
1812173297620615168 |
spelling |
Ocampo de los Ríos, Juan DavidBustamante Góez, Liliana MarcelaVallejo Ciro, María IsabelCarvajal Loaiza, Manuel José2022-01-19T21:23:19Z2022-01-19T21:23:19Z2021http://hdl.handle.net/10495/25415ABSTRACT : Fatigue failures are common failures within the aeronautical field. microcracks appear after many repetitions of cyclic stresses, then, these microcracks grow until a point of no return is reached and the growth becomes unstable and imminent. It is hard to do reliable estimations of a system subject to fatigue due to multiple random factors that affect the material, geometry, and stresses, among others. In this work, to estimate this type of failure, a probabilistic analysis is performed, where each parameter from the model is represented as a probability density function. This work presents a software application to perform fatigue failure analysis using MATLAB and SMART|DT. This last program follows the standards issued by the Federal Aviation Administration of United States (FAA). The application implements a Bayesian inference process to update the model’s crack size distribution when inspections are performed, to add more accuracy to risk predictions. This application is expected to support decisions about when to perform inspections based on an allowable desired risk for the fleet.RESUMEN : Las fallas a fatiga son fallas comunes dentro del campo aeronáutico. Luego de muchas repeticiones de esfuerzos cíclicos, microgrietas aparecen, estas crecen hasta alcanzar un punto de no retorno en el cuál terminan de crecer de manera inestable e inminente. Es difícil hacer estimaciones confiables de un sistema sujeto a fatiga debido a múltiples factores aleatorios que afectan al material, la geometría y los esfuerzos, entre otros. En este trabajo, para estimar este tipo de falla, se utiliza un análisis probabilístico, donde cada parámetro del modelo es representado como una función de densidad de probabilidad. Este trabajo presenta una aplicación para realizar análisis de falla por fatiga usando los programas MATLAB y SMART|DT, este último sigue las normas emitidas por la Administración Federal de Aviación de Los Estados Unidos (FAA), e implementa un proceso de inferencia bayesiana para actualizar la distribución de tamaño de grietas del modelo cada que se realiza una inspección para proporcionar más precisión a las predicciones de riesgo. Se espera que esta aplicación sea de soporte a la hora de tomar decisiones sobre cuando realizar inspecciones en la flota basadas en el riesgo que se quiera tomar.67application/pdfenginfo:eu-repo/semantics/draftinfo:eu-repo/semantics/bachelorThesishttp://purl.org/coar/resource_type/c_7a1fhttps://purl.org/redcol/resource_type/TPTesis/Trabajo de grado - Monografía - Pregradohttp://purl.org/coar/version/c_b1a7d7d4d402bcceinfo:eu-repo/semantics/openAccesshttp://creativecommons.org/licenses/by-nc-sa/2.5/co/http://purl.org/coar/access_right/c_abf2https://creativecommons.org/licenses/by-nc-sa/4.0/Probabilistic damage tolerance analysis using inspection data from integrated sensorsGrupo de Diseño MecánicoMedellínAeronautics - Safety measuresAeronáutica - medidas de seguridadFracture of solidsFractura de sólidosFracture strengthResistencia a las fracturasMaterials fatigueFatiga de materialesProbabilitiesProbabilidadesResidual stresseEsfuerzos residualesStability of airplanesEstabilidad de los avionesSensorsSensoresBayesian updatinghttp://aims.fao.org/aos/agrovoc/c_28279Ingeniero MecánicoPregradoFacultad de Ingeniería. Ingeniería MecánicaUniversidad de AntioquiaLICENSElicense.txtlicense.txttext/plain; charset=utf-81748https://bibliotecadigital.udea.edu.co/bitstream/10495/25415/4/license.txt8a4605be74aa9ea9d79846c1fba20a33MD54CC-LICENSElicense_rdflicense_rdfapplication/rdf+xml; charset=utf-81051https://bibliotecadigital.udea.edu.co/bitstream/10495/25415/3/license_rdfe2060682c9c70d4d30c83c51448f4eedMD53ORIGINALVallejoMaria_2021_DamageToleranceAnalysis.pdfVallejoMaria_2021_DamageToleranceAnalysis.pdfTrabajo de grado de pregradoapplication/pdf1795644https://bibliotecadigital.udea.edu.co/bitstream/10495/25415/1/VallejoMaria_2021_DamageToleranceAnalysis.pdf4f5eb882b663070e648365c53bc92f72MD51AutorizacionDePublicacion.pdfAutorizacionDePublicacion.pdfAutorización Publicaciónapplication/pdf120485https://bibliotecadigital.udea.edu.co/bitstream/10495/25415/2/AutorizacionDePublicacion.pdf9d398dd594616d24dc56cde0a69a7e81MD5210495/25415oai:bibliotecadigital.udea.edu.co:10495/254152022-01-19 16:26:41.858Repositorio Institucional Universidad de Antioquiaandres.perez@udea.edu.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 |