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    Comparative Performance of a Thermal Barrier Coating System Utilizing Platinum Aluminide Bond Coat on Alloys CMSX-4® and MAR M® 002DS

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 001::page 12101
    Author:
    H. M. Tawancy
    ,
    Luai M. Al-Hadhrami
    DOI: 10.1115/1.4004131
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is known that the relative performance of thermal barrier coatings is largely dependent upon the oxidation properties of the bond coat utilized in the system. Also, the oxidation properties of diffusion-type bond coats (aluminides and their modifications) are functions of the superalloy substrate used in blade applications. Therefore, the performance of a given coating system utilizing a diffusion-type bond coat can significantly vary from one superalloy to another. Toward the objective of developing coating systems with more universal applicability, it is essential to understand the mechanisms by which the superalloy substrate can influence the coating performance. In this study, we examined the relative performance of yttria-stabilized zirconia/platinum aluminide coating system on alloys CMSX-4 and MAR M 002DS representing single-crystal and directionally-solidified alloy systems respectively using thermal exposure tests at 1150 °C with a 24-h cycling period to room temperature. Changes in coating microstructure were characterized by various electron-optical techniques. Experiment showed that the coating system on alloy MAR M 002DS had outperformed that on alloy CMSX-4, which could be related to the high thermal stability of the bond coat on alloy MAR M 002DS. From a detailed microstructural characterization, this difference in behavior could be explained at least partially in terms of variation in chemical composition of the two alloys, which was also reflected on the exact failure mechanism of the coating system.
    keyword(s): Coating processes , Coatings , Alloys , oxidation , Platinum , Thermal barrier coatings , Thermal stability , Temperature , Superalloys , Mechanisms AND Failure mechanisms ,
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      Comparative Performance of a Thermal Barrier Coating System Utilizing Platinum Aluminide Bond Coat on Alloys CMSX-4® and MAR M® 002DS

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/148941
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorH. M. Tawancy
    contributor authorLuai M. Al-Hadhrami
    date accessioned2017-05-09T00:50:40Z
    date available2017-05-09T00:50:40Z
    date copyrightJanuary, 2012
    date issued2012
    identifier issn1528-8919
    identifier otherJETPEZ-27180#012101_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148941
    description abstractIt is known that the relative performance of thermal barrier coatings is largely dependent upon the oxidation properties of the bond coat utilized in the system. Also, the oxidation properties of diffusion-type bond coats (aluminides and their modifications) are functions of the superalloy substrate used in blade applications. Therefore, the performance of a given coating system utilizing a diffusion-type bond coat can significantly vary from one superalloy to another. Toward the objective of developing coating systems with more universal applicability, it is essential to understand the mechanisms by which the superalloy substrate can influence the coating performance. In this study, we examined the relative performance of yttria-stabilized zirconia/platinum aluminide coating system on alloys CMSX-4 and MAR M 002DS representing single-crystal and directionally-solidified alloy systems respectively using thermal exposure tests at 1150 °C with a 24-h cycling period to room temperature. Changes in coating microstructure were characterized by various electron-optical techniques. Experiment showed that the coating system on alloy MAR M 002DS had outperformed that on alloy CMSX-4, which could be related to the high thermal stability of the bond coat on alloy MAR M 002DS. From a detailed microstructural characterization, this difference in behavior could be explained at least partially in terms of variation in chemical composition of the two alloys, which was also reflected on the exact failure mechanism of the coating system.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComparative Performance of a Thermal Barrier Coating System Utilizing Platinum Aluminide Bond Coat on Alloys CMSX-4® and MAR M® 002DS
    typeJournal Paper
    journal volume134
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4004131
    journal fristpage12101
    identifier eissn0742-4795
    keywordsCoating processes
    keywordsCoatings
    keywordsAlloys
    keywordsoxidation
    keywordsPlatinum
    keywordsThermal barrier coatings
    keywordsThermal stability
    keywordsTemperature
    keywordsSuperalloys
    keywordsMechanisms AND Failure mechanisms
    treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 001
    contenttypeFulltext
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