Yasin Ozgurluk

Dr. Yasin Ozgurluk


Research Focus & Metrics

Academic Career Length

9Years (2018-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 December 2021 in Vacuum
Verified
Journal Article
Closed access
YOYasin Ozgurluk
Yasin Ozgurluk
AKAbdullah Cahit Karaoglanli
Abdullah Cahit Karaoglanli
HAHayrettin Ahlatci
Hayrettin Ahlatci

1 March 2019 in Coatings
Verified
Journal Article
Open access
PDF file
YOYasin Ozgurluk
Yasin Ozgurluk
KDKadir Mert Döleker
Kadir Mert Döleker
DODervis Ozkan
Dervis Ozkan
HAHayrettin AHLATCI
Hayrettin AHLATCI
AKAbdullah Cahit Karaoglanli
Abdullah Cahit Karaoglanli
The cold gas dynamic spray (CGDS) method has been considered a promising technology to produce a metallic bond coat for thermal barrier coating (TBC) systems. In this study, CoNiCrAlY bond coats produced by CGDS method were coated with yttria-stabilized zirconia (YSZ) by electron beam physical vapor deposition (EB-PVD). TBCs were subjected to 50 wt % V2O5 and 50 wt % Na2SO4 molten hot corrosion salt combinations at 1000 °C. In the case of YSZ top coat on TBCs, the reaction between Na2SO4, V2O5, and Y2O3 salts generates YVO4 crystals, and these structures cause the transformation of tetragonal ZrO2 to monoclinic ZrO2. This situation occurs under operating conditions that lead to TBC failure. Hot corrosion behavior and the related failure mechanisms of TBC systems were investigated and discussed using scanning electron microscope (SEM), energy dispersive spectroscopy (EDS) analysis, and X-ray diffractometer (XRD).

2 June 2018 in Arabian Journal of Geosciences
Verified
Journal Article
Closed access
PDF file
YOYasin Ozgurluk
Yasin Ozgurluk
KDKadir Mert Döleker
Kadir Mert Döleker
HAHayrettin Ahlatci
Hayrettin Ahlatci
AKAbdullah Cahit Karaoglanli
Abdullah Cahit Karaoglanli

1 January 2018 in Open Chemistry
Verified
Journal Article
Open access
PDF file
YOYasin Ozgurluk
Yasin Ozgurluk
KDKadir Mert Döleker
Kadir Mert Döleker
HAHayrettin Ahlatci
Hayrettin Ahlatci
DODervis Ozkan
Dervis Ozkan
AKAbdullah Cahit Karaoglanli
Abdullah Cahit Karaoglanli
Thermal barrier coatings (TBCs) are widely used in aerospace and aviation industries for materials required to withstand severe environments such as oxidation, hot-corrosion failure and CMAS (calcia–magnesia–alumina–silica) attack or vermiculite corrosion. This is particularly apparent in vermiculite, which can penetrate sand, volcanic ash and is the most destructive damage mechanism in the TBC system. Impurities from the desert environment such as calcia–magnesia–alumina–silica (CMAS) cause degradation of TBCs. In this research, CoNiCrAlY metallic bond coatings were deposited on Inconel 718 nickel based superalloy substrates with a thickness of around 100 μm using a Cold Gas Dynamic Spray (CGDS) technique. Production of TBCs were carried out with deposition of YSZ ceramic top coating material using Electron Beam Physical Vapor Deposition (EB-PVD), with a thickness of around 200 μm. The effect of CMAS with spreading naturally-occurring mineral (vermiculite) on TBC samples were investigated using scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS) analysis and X-ray diffraction (XRD). The microstructure evolution of YSZ and failure mechanism of TBC were evaluated.

20 May 2018
Verified
Book Chapter
Closed access
PDF file
MKMustafa Kaplan
Mustafa Kaplan
MUMesut Uyaner
Mesut Uyaner
YOYasin Ozgurluk
Yasin Ozgurluk
KDKadir Mert Döleker
Kadir Mert Döleker
AKAbdullah Cahit Karaoglanli
Abdullah Cahit Karaoglanli

28 May 2024 in Journal of Materials Engineering and Performance
Verified
Journal Article
Closed access
PDF file
DODervis Ozkan
Dervis Ozkan
AGAhmet Gulec
Ahmet Gulec
MOMecit Oge
Mecit Oge
YOYasin Ozgurluk
Yasin Ozgurluk
GBGulfem Binal
Gulfem Binal
AKAbdullah Cahit Karaoglanli
Abdullah Cahit Karaoglanli