Evaluation of oxidation and thermal cyclic behavior of YSZ, Gd2Zr2O7 and YSZ/Gd2Zr2O7 TBCs

dc.contributor.authorDoleker, Kadir Mert
dc.contributor.authorOzgurluk, Yasin
dc.contributor.authorAhlatci, Hayrettin
dc.contributor.authorKaraoğlanlı, Abdullah Cahit
dc.contributor.authorÖzgürlük, Yasin
dc.contributor.authorKaraoğlanlı, Abdullah Cahit
dc.date.accessioned2025-10-18T13:22:40Z
dc.date.created2019
dc.date.issued2019
dc.departmentFakülteler, Mühendislik Mimarlık ve Tasarım Fakültesi, Metalurji ve Malzemem Mühendisliği Bölümü
dc.description8th International Meeting of Thermal Projection (RIPT) -- DEC 06-08, 2017 -- Limoges, FRANCE
dc.description.abstractThermal barrier coatings (TBCs) are widely used to increase gas turbine efficiency and to prolong the lifetimes of superalloy substrates. Yttria (7-8%) stabilized zirconia (YSZ) is used as a state of the art TBC top coating material. In recent years, rare earth zirconates have drawn interest as top coating materials due to their high phase transformation temperature and low thermal conductivity. In the present research, CoNiCrAlY powders were sprayed on Inconel 718 superalloy substrates using high velocity oxy fuel (HVOF) deposition technique. YSZ, Gd2Zr2O7 (GZ) and YSZ/GZ top coats were then deposited on the resulting bond coat using EB-PVD technique. The produced TBCs were exposed to isothermal oxidation at 1100 degrees C for 4 different periods, and furnace thermal cyclic tests were conducted at 1150 degrees C. After thermal loadings, TGO (thermally grown oxide) growth behavior and crack surfaces of TBCs were evaluated. Samples were compared with each other using analysis techniques like scanning electron microscopy (SEM), energy dispersive sprectrum (EDS) elemental mapping and X-ray diffraction (XRD) before and after the oxidation tests. The results showed that double layered TBC system is more durable against high temperature degradations.
dc.description.sponsorshipScientific and Technological Research Council of Turkey (TUBITAK) [113R049]; Scientific Research Projects (BAP) Coordinator ship of Karabuk University [KBUBAP-17-DR-202]
dc.description.sponsorshipThis investigation was financially supported by The Scientific and Technological Research Council of Turkey (TUBITAK, 113R049) and Scientific Research Projects (BAP) Coordinator ship of Karabuk University with project code of KBUBAP-17-DR-202.
dc.identifier.doi10.1016/j.surfcoat.2018.11.055
dc.identifier.endpage275
dc.identifier.issn0257-8972
dc.identifier.issn1879-3347
dc.identifier.orcidDoleker, Kadir Mert/0000-0003-4057-6832;
dc.identifier.scopus2-s2.0-85057041444
dc.identifier.scopusqualityQ1
dc.identifier.startpage262
dc.identifier.urihttps://doi.org/10.1016/j.surfcoat.2018.11.055
dc.identifier.urihttps://hdl.handle.net/11772/22465
dc.identifier.volume371
dc.identifier.wosWOS:000472694300028
dc.identifier.wosqualityQ1
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherElsevier Science Sa
dc.relation.ispartofSurface & Coatings Technology
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzWoS_20251016
dc.subjectThermal Barrier Coating (Tbc)
dc.subjectHigh Velocity Oxygen Fuel (Hvof)
dc.subjectOxidation
dc.subjectThermal Cyclic
dc.subjectYsz
dc.subjectGd2zr2o7 (Gz)
dc.titleEvaluation of oxidation and thermal cyclic behavior of YSZ, Gd2Zr2O7 and YSZ/Gd2Zr2O7 TBCs
dc.typeConference Object
dspace.entity.typePublication
relation.isAuthorOfPublicationa32e3510-fcaa-42b3-baf9-8d10347abf2b
relation.isAuthorOfPublication529d50c7-6643-4720-a7f6-8aaebba59292
relation.isAuthorOfPublication.latestForDiscoverya32e3510-fcaa-42b3-baf9-8d10347abf2b

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