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    Thermal Barrier Coating Life Prediction Model Development

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002::page 258
    Author:
    S. M. Meier
    ,
    T. A. Cruse
    ,
    D. M. Nissley
    ,
    K. D. Sheffler
    DOI: 10.1115/1.2906581
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A thermal barrier coated (TBC) turbine component design system, including an accurate TBC life prediction model, is needed to realize the full potential of available TBC engine performance and/or durability benefits. The objective of this work, which was sponsored in part by NASA under the Hot Section Technology (HOST) Program (Contract NAS3-23944), was to generate a life prediction model for electron beam-physical vapor deposited (EB-PVD) zirconia TBC. Specific results include EB-PVD zirconia mechanical and physical properties, coating adherence strength measurements, interfacial oxide growth characteristics, quantitative cyclic thermal spallation life data, and a spallation life model.
    keyword(s): Electrons , Vapors , Coating processes , Coatings , Measurement , Engines , Spallation (Nuclear physics) , Design , Durability , Turbine components , Model development AND Thermal barrier coatings ,
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      Thermal Barrier Coating Life Prediction Model Development

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/110233
    Collections
    • Journal of Engineering for Gas Turbines and Power

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    contributor authorS. M. Meier
    contributor authorT. A. Cruse
    contributor authorD. M. Nissley
    contributor authorK. D. Sheffler
    date accessioned2017-05-08T23:38:26Z
    date available2017-05-08T23:38:26Z
    date copyrightApril, 1992
    date issued1992
    identifier issn1528-8919
    identifier otherJETPEZ-26699#258_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110233
    description abstractA thermal barrier coated (TBC) turbine component design system, including an accurate TBC life prediction model, is needed to realize the full potential of available TBC engine performance and/or durability benefits. The objective of this work, which was sponsored in part by NASA under the Hot Section Technology (HOST) Program (Contract NAS3-23944), was to generate a life prediction model for electron beam-physical vapor deposited (EB-PVD) zirconia TBC. Specific results include EB-PVD zirconia mechanical and physical properties, coating adherence strength measurements, interfacial oxide growth characteristics, quantitative cyclic thermal spallation life data, and a spallation life model.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThermal Barrier Coating Life Prediction Model Development
    typeJournal Paper
    journal volume114
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906581
    journal fristpage258
    journal lastpage263
    identifier eissn0742-4795
    keywordsElectrons
    keywordsVapors
    keywordsCoating processes
    keywordsCoatings
    keywordsMeasurement
    keywordsEngines
    keywordsSpallation (Nuclear physics)
    keywordsDesign
    keywordsDurability
    keywordsTurbine components
    keywordsModel development AND Thermal barrier coatings
    treeJournal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002
    contenttypeFulltext
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