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    Simulations of Multiphase Particle Deposition on a Gas Turbine Endwall With Impingement and Film Cooling

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 011::page 111002
    Author:
    Mensch, Amy
    ,
    Thole, Karen
    DOI: 10.1115/1.4031177
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Replacing natural gas fuels with coalderived syngas in industrial gas turbines can lead to molten particle deposition on the turbine components. The deposition of the particles, which originate from impurities in the syngas fuels, can increase surface roughness and obstruct film cooling holes. These deposition effects increase heat transfer to the components and degrade the performance of cooling mechanisms, which are critical for maintaining component life. The current experimental study dynamically simulated molten particle deposition on a conducting blade endwall with the injection of molten wax. The key nondimensional parameters for modeling of conjugate heat transfer and deposition were replicated in the experiment. The endwall was cooled with internal impingement jet cooling and film cooling. Increasing blowing ratio mitigated some deposition at the film cooling hole exits and in areas of coolest endwall temperatures. After deposition, the external surface temperatures and internal endwall temperatures were measured and found to be warmer than the endwall temperatures measured before deposition. Although the deposition helps insulate the endwall from the mainstream, the roughness effects of the deposition counteract the insulating effect by decreasing the benefit of film cooling and by increasing external heat transfer coefficients.
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      Simulations of Multiphase Particle Deposition on a Gas Turbine Endwall With Impingement and Film Cooling

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    http://yetl.yabesh.ir/yetl1/handle/yetl/159984
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    contributor authorMensch, Amy
    contributor authorThole, Karen
    date accessioned2017-05-09T01:24:47Z
    date available2017-05-09T01:24:47Z
    date issued2015
    identifier issn0889-504X
    identifier otherturbo_137_11_111002.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159984
    description abstractReplacing natural gas fuels with coalderived syngas in industrial gas turbines can lead to molten particle deposition on the turbine components. The deposition of the particles, which originate from impurities in the syngas fuels, can increase surface roughness and obstruct film cooling holes. These deposition effects increase heat transfer to the components and degrade the performance of cooling mechanisms, which are critical for maintaining component life. The current experimental study dynamically simulated molten particle deposition on a conducting blade endwall with the injection of molten wax. The key nondimensional parameters for modeling of conjugate heat transfer and deposition were replicated in the experiment. The endwall was cooled with internal impingement jet cooling and film cooling. Increasing blowing ratio mitigated some deposition at the film cooling hole exits and in areas of coolest endwall temperatures. After deposition, the external surface temperatures and internal endwall temperatures were measured and found to be warmer than the endwall temperatures measured before deposition. Although the deposition helps insulate the endwall from the mainstream, the roughness effects of the deposition counteract the insulating effect by decreasing the benefit of film cooling and by increasing external heat transfer coefficients.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimulations of Multiphase Particle Deposition on a Gas Turbine Endwall With Impingement and Film Cooling
    typeJournal Paper
    journal volume137
    journal issue11
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4031177
    journal fristpage111002
    journal lastpage111002
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2015:;volume( 137 ):;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
    yabeshDSpacePersian