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    Determination of Thermal Barrier Coatings Average Surface Temperature After Engine Operation for Lifetime Validation

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 012::page 122507
    Author:
    Grégoire Witz
    ,
    Hans-Peter Bossmann
    DOI: 10.1115/1.4007343
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Assessment of ex-service parts is important for the power generation industry. It gives us the opportunity to correlate part conditions to specific operating conditions like fuel used, local atmospheric conditions, operating regime, and temperature load. For assessment of thermal barrier coatings, one of the most valuable pieces of information is the local thermal condition. A method has been developed in Alstom, allowing determination of a thermal barrier coating average surface temperature after engine operation. It is based on the analysis of the phase composition of the thermal barrier coating by the acquisition of an X-ray diffraction spectrum of the coating surface, and its analysis using Rietveld refinement. The method has been validated by comparing its outcome to thermal models and base metal temperature mapping data. It is used for assessment of combustor and turbine coatings with various purposes: Determination of remnant coating life, building of lifing models, or determination of the coating degradation mechanisms under some specific operating conditions. Examples will be presented showing applications of this method.
    keyword(s): Temperature , Engines , Thermal barrier coatings AND Mechanisms ,
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      Determination of Thermal Barrier Coatings Average Surface Temperature After Engine Operation for Lifetime Validation

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/148692
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorGrégoire Witz
    contributor authorHans-Peter Bossmann
    date accessioned2017-05-09T00:49:48Z
    date available2017-05-09T00:49:48Z
    date copyright41244
    date issued2012
    identifier issn1528-8919
    identifier otherJETPEZ-926523#gtp_134_12_122507.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148692
    description abstractAssessment of ex-service parts is important for the power generation industry. It gives us the opportunity to correlate part conditions to specific operating conditions like fuel used, local atmospheric conditions, operating regime, and temperature load. For assessment of thermal barrier coatings, one of the most valuable pieces of information is the local thermal condition. A method has been developed in Alstom, allowing determination of a thermal barrier coating average surface temperature after engine operation. It is based on the analysis of the phase composition of the thermal barrier coating by the acquisition of an X-ray diffraction spectrum of the coating surface, and its analysis using Rietveld refinement. The method has been validated by comparing its outcome to thermal models and base metal temperature mapping data. It is used for assessment of combustor and turbine coatings with various purposes: Determination of remnant coating life, building of lifing models, or determination of the coating degradation mechanisms under some specific operating conditions. Examples will be presented showing applications of this method.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDetermination of Thermal Barrier Coatings Average Surface Temperature After Engine Operation for Lifetime Validation
    typeJournal Paper
    journal volume134
    journal issue12
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4007343
    journal fristpage122507
    identifier eissn0742-4795
    keywordsTemperature
    keywordsEngines
    keywordsThermal barrier coatings AND Mechanisms
    treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 012
    contenttypeFulltext
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