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    Coating Life Prediction for Combustion Turbine Blades

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003::page 484
    Author:
    K. S. Chan
    ,
    N. S. Cheruvu
    ,
    G. R. Leverant
    DOI: 10.1115/1.2818498
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A life prediction method for combustion turbine blade coatings has been developed by modeling coating degradation mechanisms including oxidation, spallation, and aluminum loss due to inward diffusion. Using this model, the influence of cycle time on coating life is predicted for GTD-111 coated with an MCrAlY, PtAl, or aluminide coating. The results are used to construct a coating life diagram that depicts failure and safe regions for the coating in a log-log Plot of number of startup cycles versus cycle time. The regime where failure by oxidation, spallation, and inward diffusion dominates is identified and delineated from that dominated by oxidation and inward diffusion only. A procedure for predicting the remaining life of a coating is developed. The utility of the coating life diagram for predicting the failure and useful life of MCrAlY, aluminide, or PtAl coatings on the GTD-111 substrate is illustrated and compared against experimental data.
    keyword(s): Coating processes , Coatings , Turbine blades , Combustion , Diffusion (Physics) , Cycles , Failure , oxidation , Spallation (Nuclear physics) , Modeling , Mechanisms AND Aluminum ,
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      Coating Life Prediction for Combustion Turbine Blades

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/122124
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorK. S. Chan
    contributor authorN. S. Cheruvu
    contributor authorG. R. Leverant
    date accessioned2017-05-08T23:59:34Z
    date available2017-05-08T23:59:34Z
    date copyrightJuly, 1999
    date issued1999
    identifier issn1528-8919
    identifier otherJETPEZ-26790#484_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122124
    description abstractA life prediction method for combustion turbine blade coatings has been developed by modeling coating degradation mechanisms including oxidation, spallation, and aluminum loss due to inward diffusion. Using this model, the influence of cycle time on coating life is predicted for GTD-111 coated with an MCrAlY, PtAl, or aluminide coating. The results are used to construct a coating life diagram that depicts failure and safe regions for the coating in a log-log Plot of number of startup cycles versus cycle time. The regime where failure by oxidation, spallation, and inward diffusion dominates is identified and delineated from that dominated by oxidation and inward diffusion only. A procedure for predicting the remaining life of a coating is developed. The utility of the coating life diagram for predicting the failure and useful life of MCrAlY, aluminide, or PtAl coatings on the GTD-111 substrate is illustrated and compared against experimental data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCoating Life Prediction for Combustion Turbine Blades
    typeJournal Paper
    journal volume121
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2818498
    journal fristpage484
    journal lastpage488
    identifier eissn0742-4795
    keywordsCoating processes
    keywordsCoatings
    keywordsTurbine blades
    keywordsCombustion
    keywordsDiffusion (Physics)
    keywordsCycles
    keywordsFailure
    keywordsoxidation
    keywordsSpallation (Nuclear physics)
    keywordsModeling
    keywordsMechanisms AND Aluminum
    treeJournal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003
    contenttypeFulltext
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