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    Extreme Temperature Coatings for Future Gas Turbine Engines

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 011::page 112102
    Author:
    Alvin, M. A.
    ,
    Klotz, K.
    ,
    McMordie, B.
    ,
    Zhu, D.
    ,
    Gleeson, B.
    ,
    Warnes, B.
    DOI: 10.1115/1.4027186
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The National Energy Technology LaboratoryRegional University Alliance (NETLRUA) has been developing extreme temperature coating systems that consist of a diffusion barrier coating (DBC), a lowcost wet slurry bond coat, a commercial yttria stabilized zirconia (YSZ) thermal barrier coating (TBC), and an extreme temperature external coating that are deposited along the surface of nickelbased superalloys and single crystal metal substrates. Thermal cyclic testing of these multilayer coatings was conducted in steamcontaining environments at temperatures ranging between 1100 and 1550 آ°C. This paper discusses the response of these materials during benchscale testing, and their potential use in advanced Hand Jclass landbased gas turbine engines.
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      Extreme Temperature Coatings for Future Gas Turbine Engines

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/154844
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorAlvin, M. A.
    contributor authorKlotz, K.
    contributor authorMcMordie, B.
    contributor authorZhu, D.
    contributor authorGleeson, B.
    contributor authorWarnes, B.
    date accessioned2017-05-09T01:08:05Z
    date available2017-05-09T01:08:05Z
    date issued2014
    identifier issn1528-8919
    identifier othergtp_136_11_112102.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154844
    description abstractThe National Energy Technology LaboratoryRegional University Alliance (NETLRUA) has been developing extreme temperature coating systems that consist of a diffusion barrier coating (DBC), a lowcost wet slurry bond coat, a commercial yttria stabilized zirconia (YSZ) thermal barrier coating (TBC), and an extreme temperature external coating that are deposited along the surface of nickelbased superalloys and single crystal metal substrates. Thermal cyclic testing of these multilayer coatings was conducted in steamcontaining environments at temperatures ranging between 1100 and 1550 آ°C. This paper discusses the response of these materials during benchscale testing, and their potential use in advanced Hand Jclass landbased gas turbine engines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExtreme Temperature Coatings for Future Gas Turbine Engines
    typeJournal Paper
    journal volume136
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4027186
    journal fristpage112102
    journal lastpage112102
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 011
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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