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...

Full description

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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network_acronym_str UDEA2
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repository_id_str
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
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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/
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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/
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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
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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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