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Degradation of YSZ/EUCOR TBC Coating System during High Temperature Low Cycle Fatigue Tests

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68081723%3A_____%2F17%3A00465121" target="_blank" >RIV/68081723:_____/17:00465121 - isvavai.cz</a>

  • Alternative codes found

    RIV/00216305:26620/17:PU121343

  • Result on the web

    <a href="http://dx.doi.org/10.4028/www.scientific.net/SSP.258.420" target="_blank" >http://dx.doi.org/10.4028/www.scientific.net/SSP.258.420</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.4028/www.scientific.net/SSP.258.420" target="_blank" >10.4028/www.scientific.net/SSP.258.420</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Degradation of YSZ/EUCOR TBC Coating System during High Temperature Low Cycle Fatigue Tests

  • Original language description

    Thermal barrier coatings are widely used to protect the substrate from high temperature and extremely aggressive environments in gas engines. In the present article, authors have been studied degradation of complex thermal barrier coating system deposited on polycrystalline nickel superalloy IN 713LC. The substrate material was grit blasted with alumina (Al2O3) particles prior to air plasma deposition of CoNiCrAlY bond coat. Top coat consists of conventional zirconia (ZrO2) stabilized by yttria (Y2O3) -YSZ ceramic in combination with a eutectic nanocrystalline ceramic Eucor made of zirconia (ZrO2), alumina (Al2O3) and silicia (SiO2) –in the ratio of 50/50 in wt. %. The top coat was deposited using water stabilized plasma. Test specimens with the TBC coating system were fatigued under strain control condition in fully reversed symmetrical push-pull cycles at 900°C in air. The microstructure of TBC was characterized with scanning electron microscopy and energy dispersion X-ray analysis. The coating hardness and thickness were measured. Fracture surface and polished sections parallel to the specimen axis were examined to study damage mechanisms in coatings under cyclic loading at high temperature. TBC delamination was observed at the top coat/bond coat interface after cyclic loading at high temperature. Fatigue crack initiation sites are documented. Majority of fatigue cracks start from the surface and top coat/bond coat interface.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20306 - Audio engineering, reliability analysis

Result continuities

  • Project

    Result was created during the realization of more than one project. More information in the Projects tab.

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2017

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    Materials Structure & Micromechanics of Fracture VIII

  • ISBN

    978-3-03835-626-4

  • ISSN

    1662-9779

  • e-ISSN

  • Number of pages

    4

  • Pages from-to

    420-423

  • Publisher name

    Trans Tech Publications

  • Place of publication

    Zürrich

  • Event location

    Brno

  • Event date

    Jun 27, 2016

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article