Failure analysis of J85-CAN-15 turbojet engine compressor disc

dc.authoridhttps://orcid.org/0000-0001-5338-726Xen_US
dc.contributor.authorSaraçyakupoğlu, Tamer
dc.date.accessioned2023-06-13T19:50:54Z
dc.date.available2023-06-13T19:50:54Z
dc.date.issued2021en_US
dc.departmentMühendislik ve Mimarlık Fakültesien_US
dc.description.abstractThis paper analyzes the J85-CAN-15 engine damage due to fracture of the compressor disc 8th stage dovetail post. An Inner Object Damage (IOD) phenomenon was identified. The damaged compressor disc material is Incoloy 901 forging. The composition of the disc is determined as 42.7%-Ni, 34%-Fe, 13.5%-Cr, 6.2% Mo, 2.5%Ti, 0.1%-Cu, and 0.05%-C. The average hardness value of the material is 44 HRC. The burrs have been observed under Field Emission Scanning Electron Microscope (SEM) and they are considered as the origin of the fatigue on the engine compressor disc. The metallurgical analysis results show that manufacturing defect was propagated under the repeated low and high cyclic loads.en_US
dc.identifier.doi10.1016/j.engfailanal.2020.104975en_US
dc.identifier.endpage8en_US
dc.identifier.issn1350-6307
dc.identifier.issn1873-1961
dc.identifier.scopus2-s2.0-85092275428en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage1en_US
dc.identifier.urihttps://hdl.handle.net/11363/4887
dc.identifier.urihttps://doi.org/
dc.identifier.volume119en_US
dc.identifier.wosWOS:000597337600002en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.institutionauthorSaraçyakupoğlu, Tamer
dc.language.isoenen_US
dc.publisherPERGAMON-ELSEVIER SCIENCE LTD, THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLANDen_US
dc.relation.ispartofEngineering Failure Analysisen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
dc.subjectJ85-CAN-15en_US
dc.subjectDovetail posten_US
dc.subjectFatigue failureen_US
dc.subjectCracken_US
dc.subjectManufacturing defecten_US
dc.titleFailure analysis of J85-CAN-15 turbojet engine compressor discen_US
dc.typeArticleen_US

Dosyalar

Orijinal paket
Listeleniyor 1 - 1 / 1
Yükleniyor...
Küçük Resim
İsim:
1-s2.0-S1350630720314990-main.pdf
Boyut:
12.97 MB
Biçim:
Adobe Portable Document Format
Açıklama:
Makale / Article
Lisans paketi
Listeleniyor 1 - 1 / 1
[ N/A ]
İsim:
license.txt
Boyut:
1.56 KB
Biçim:
Item-specific license agreed upon to submission
Açıklama: