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    Microstructural Features Resulting From Isothermal and Thermocyclic Exposure of a Thermal Barrier Coating

    Source: Journal of Engineering Materials and Technology:;2000:;volume( 122 ):;issue: 003::page 333
    Author:
    Mark E. Walter
    ,
    Bolarinwa Onipede
    ,
    Wole Soboyejo
    ,
    Chris Mercer
    DOI: 10.1115/1.482805
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Thermal barrier coating (TBC) systems are receiving a great deal of attention as a result of their ability to enable higher operating temperatures without sacrificing component durability in gas turbine systems. Nonetheless, there are a number of unknowns associated with the failure of TBC systems. In particular, the initiation and propagation of damage has not been observed. In this paper, the microstructural changes in and along the thermally growth oxide layer of a TBC are presented. Specimens were studied primarily after isothermal exposure for 48, 96, 200, and 300 hours at 1100°C and also after thermocyclic exposure. Failure features are discussed and the growth of oxide is quantified. The oxide growth is placed within the context of a parabolic growth model. [S0094-4289(00)01503-6]
    keyword(s): Gas turbines , Failure , Thermal barrier coatings , Thickness , Fracture (Materials) , Diffusion (Physics) , Product quality , Coating processes , Coatings , Durability AND Operating temperature ,
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      Microstructural Features Resulting From Isothermal and Thermocyclic Exposure of a Thermal Barrier Coating

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    https://yetl.yabesh.ir/yetl1/handle/yetl/123764
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    contributor authorMark E. Walter
    contributor authorBolarinwa Onipede
    contributor authorWole Soboyejo
    contributor authorChris Mercer
    date accessioned2017-05-09T00:02:33Z
    date available2017-05-09T00:02:33Z
    date copyrightJuly, 2000
    date issued2000
    identifier issn0094-4289
    identifier otherJEMTA8-27009#333_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123764
    description abstractThermal barrier coating (TBC) systems are receiving a great deal of attention as a result of their ability to enable higher operating temperatures without sacrificing component durability in gas turbine systems. Nonetheless, there are a number of unknowns associated with the failure of TBC systems. In particular, the initiation and propagation of damage has not been observed. In this paper, the microstructural changes in and along the thermally growth oxide layer of a TBC are presented. Specimens were studied primarily after isothermal exposure for 48, 96, 200, and 300 hours at 1100°C and also after thermocyclic exposure. Failure features are discussed and the growth of oxide is quantified. The oxide growth is placed within the context of a parabolic growth model. [S0094-4289(00)01503-6]
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMicrostructural Features Resulting From Isothermal and Thermocyclic Exposure of a Thermal Barrier Coating
    typeJournal Paper
    journal volume122
    journal issue3
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.482805
    journal fristpage333
    journal lastpage337
    identifier eissn1528-8889
    keywordsGas turbines
    keywordsFailure
    keywordsThermal barrier coatings
    keywordsThickness
    keywordsFracture (Materials)
    keywordsDiffusion (Physics)
    keywordsProduct quality
    keywordsCoating processes
    keywordsCoatings
    keywordsDurability AND Operating temperature
    treeJournal of Engineering Materials and Technology:;2000:;volume( 122 ):;issue: 003
    contenttypeFulltext
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