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    Hot Corrosion of Lanthanum Zirconate and Partially Stabilized Zirconia Thermal Barrier Coatings

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 001::page 144
    Author:
    Basil R. Marple
    ,
    Douglas R. Nagy
    ,
    Robert Vassen
    ,
    Joël Voyer
    ,
    Michel Thibodeau
    DOI: 10.1115/1.1924534
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The hot corrosion resistance of lanthanum zirconate and 8wt.% yttria-stabilized zirconia coatings produced by thermal spraying for use as thermal barriers on industrial gas turbines or in aerospace applications was evaluated. The two ceramic oxide coatings were exposed for various periods of time at temperatures up to 1000°C to vanadium- and sulfur-containing compounds, species often produced during the combustion of typical fuels used in these applications. Changes in the coatings were studied using a scanning electron microscope to observe the microstructure and x-ray diffraction techniques to analyze the phase composition. The results showed different behaviors for the two materials: the zirconia-based coating being rapidly degraded by the vanadium compounds and resistant to attack by the sulfur materials while the lanthanum zirconate was less damaged by exposure to vanadia but severely attacked in the presence of sulfur-containing species.
    keyword(s): Coating processes , Coatings , Corrosion , Lanthanum , Zirconium , Sulfur , Sulfur compounds AND Thermal barrier coatings ,
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      Hot Corrosion of Lanthanum Zirconate and Partially Stabilized Zirconia Thermal Barrier Coatings

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/133729
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorBasil R. Marple
    contributor authorDouglas R. Nagy
    contributor authorRobert Vassen
    contributor authorJoël Voyer
    contributor authorMichel Thibodeau
    date accessioned2017-05-09T00:19:56Z
    date available2017-05-09T00:19:56Z
    date copyrightJanuary, 2006
    date issued2006
    identifier issn1528-8919
    identifier otherJETPEZ-26894#144_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133729
    description abstractThe hot corrosion resistance of lanthanum zirconate and 8wt.% yttria-stabilized zirconia coatings produced by thermal spraying for use as thermal barriers on industrial gas turbines or in aerospace applications was evaluated. The two ceramic oxide coatings were exposed for various periods of time at temperatures up to 1000°C to vanadium- and sulfur-containing compounds, species often produced during the combustion of typical fuels used in these applications. Changes in the coatings were studied using a scanning electron microscope to observe the microstructure and x-ray diffraction techniques to analyze the phase composition. The results showed different behaviors for the two materials: the zirconia-based coating being rapidly degraded by the vanadium compounds and resistant to attack by the sulfur materials while the lanthanum zirconate was less damaged by exposure to vanadia but severely attacked in the presence of sulfur-containing species.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHot Corrosion of Lanthanum Zirconate and Partially Stabilized Zirconia Thermal Barrier Coatings
    typeJournal Paper
    journal volume128
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1924534
    journal fristpage144
    journal lastpage152
    identifier eissn0742-4795
    keywordsCoating processes
    keywordsCoatings
    keywordsCorrosion
    keywordsLanthanum
    keywordsZirconium
    keywordsSulfur
    keywordsSulfur compounds AND Thermal barrier coatings
    treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 001
    contenttypeFulltext
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