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    Inhibition of Interdiffusion From MCrAlY Overlay Coatings by Application of a Ni-Re Interlayer

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 002::page 313
    Author:
    R. A. Page
    ,
    G. R. Leverant
    DOI: 10.1115/1.2817122
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The durability of protective coatings on combustion turbine blades and vanes is a critical issue in the power generation industry. Coating life usually dictates the refurbishment intervals for these components, and these intervals have generally been of shorter duration than desired by the operators of the equipment. Both MCrAlY and aluminide type coatings protect against oxidation and hot corrosion by forming a protective Al2 O3 surface layer. Degradation of the coatings occurs by depletion of the aluminum content of the coating through interdiffusion with the substrate and through the formation and spallation of an external Al2 O3 scale. The results obtained in this study clearly show that the application of a thin interlayer of Ni-Re beneath the MCrAlY coating can significantly decrease the growth rate of the inner β-NiAl depletion zone. Order of magnitude reductions in the inner depletion zone thickness formed at 1000 h were obtained with both the Ni-32 wt.% Re and the Ni-47 wt.% Re interlayer coatings. Since formation of the inner depletion zone is believed to result from interdiffusion with the substrate, these results suggest that the Ni-Re interlayer provided a significant impediment to the inward diffusion of Al into the substrate.
    keyword(s): Diffusion (Physics) , Combustion , Aluminum , Coating processes , Coatings , Overlays (Materials engineering) , Turbine blades , Spallation (Nuclear physics) , Corrosion , Durability , Energy generation , Electric power generation , oxidation , Protective coatings AND Thickness ,
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      Inhibition of Interdiffusion From MCrAlY Overlay Coatings by Application of a Ni-Re Interlayer

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    http://yetl.yabesh.ir/yetl1/handle/yetl/122158
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorR. A. Page
    contributor authorG. R. Leverant
    date accessioned2017-05-08T23:59:38Z
    date available2017-05-08T23:59:38Z
    date copyrightApril, 1999
    date issued1999
    identifier issn1528-8919
    identifier otherJETPEZ-26788#313_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122158
    description abstractThe durability of protective coatings on combustion turbine blades and vanes is a critical issue in the power generation industry. Coating life usually dictates the refurbishment intervals for these components, and these intervals have generally been of shorter duration than desired by the operators of the equipment. Both MCrAlY and aluminide type coatings protect against oxidation and hot corrosion by forming a protective Al2 O3 surface layer. Degradation of the coatings occurs by depletion of the aluminum content of the coating through interdiffusion with the substrate and through the formation and spallation of an external Al2 O3 scale. The results obtained in this study clearly show that the application of a thin interlayer of Ni-Re beneath the MCrAlY coating can significantly decrease the growth rate of the inner β-NiAl depletion zone. Order of magnitude reductions in the inner depletion zone thickness formed at 1000 h were obtained with both the Ni-32 wt.% Re and the Ni-47 wt.% Re interlayer coatings. Since formation of the inner depletion zone is believed to result from interdiffusion with the substrate, these results suggest that the Ni-Re interlayer provided a significant impediment to the inward diffusion of Al into the substrate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInhibition of Interdiffusion From MCrAlY Overlay Coatings by Application of a Ni-Re Interlayer
    typeJournal Paper
    journal volume121
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2817122
    journal fristpage313
    journal lastpage319
    identifier eissn0742-4795
    keywordsDiffusion (Physics)
    keywordsCombustion
    keywordsAluminum
    keywordsCoating processes
    keywordsCoatings
    keywordsOverlays (Materials engineering)
    keywordsTurbine blades
    keywordsSpallation (Nuclear physics)
    keywordsCorrosion
    keywordsDurability
    keywordsEnergy generation
    keywordsElectric power generation
    keywordsoxidation
    keywordsProtective coatings AND Thickness
    treeJournal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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