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Failure Analysis of Jet Engine Turbine Blade

dc.creatorJovanović, Milan T.
dc.creatorMaksimović, Vesna
dc.creatorCvijović-Alagić, Ivana
dc.date.accessioned2018-03-01T16:50:01Z
dc.date.available2018-03-01T16:50:01Z
dc.date.issued2016
dc.identifier.issn2217-8961
dc.identifier.urihttps://vinar.vin.bg.ac.rs/handle/123456789/1030
dc.description.abstractJet engine turbine blade cast by investment precision casting of Ni-base superalloy, which failed during exploatation, was the subject of investigation. Failure analysis was executed applying optical microscopy (OM), transmission electron microscopy (TEM) using replica technique, scaning electron microscopy (SEM) and stress rupture life tests. On the ground of obtained results it was concluded that the failure occurred as a result of structural changes caused by turbine blade overheating above the exploitation temperature.en
dc.relationinfo:eu-repo/grantAgreement/MESTD/Integrated and Interdisciplinary Research (IIR or III)/45012/RS//
dc.relationinfo:eu-repo/grantAgreement/MESTD/Basic Research (BR or ON)/174004/RS//
dc.rightsopenAccessen
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.sourceMetallurgical and Materials Engineeringen
dc.subjectJet engine turbine bladeen
dc.subjectNi-base superalloyen
dc.subjectFailureen
dc.subjectMicrostructural characterizationen
dc.subjectTEMen
dc.subjectStress rupture lifeen
dc.titleFailure Analysis of Jet Engine Turbine Bladeen
dc.typearticleen
dc.rights.licenseBY
dcterms.abstractЈовановиц, Милан Т.; Максимовић Весна; Цвијовић-Aлагић Ивана;
dc.citation.volume22
dc.citation.issue1
dc.citation.spage31
dc.citation.epage37
dc.identifier.wos000374473600005
dc.identifier.doi10.30544/138
dc.citation.rankM24
dc.type.versionpublishedVersion
dc.identifier.fulltexthttps://vinar.vin.bg.ac.rs/bitstream/id/23986/bitstream_23986.pdf


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