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    Convection in Scaled Turbine Internal Cooling Passages With Additive Manufacturing Roughness

    Source: Journal of Turbomachinery:;2021:;volume( 144 ):;issue: 004::page 41008-1
    Author:
    Stafford, Gabriel J.
    ,
    McClain, Stephen T.
    ,
    Hanson, David R.
    ,
    Kunz, Robert F.
    ,
    Thole, Karen A.
    DOI: 10.1115/1.4052524
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Additive manufacturing processes, such as direct metal laser sintering (DMLS), enable the creation of novel turbine cooling internal passages and systems. However, the DMLS method produces a significant and unique surface roughness. Previous work in scaled passages analyzed pressure losses and friction factors associated with the rough surfaces, as well as investigated the velocity profiles and turbulent flow characteristics within the passage. In this study, the heat transfer characteristics of scaled additively manufactured surfaces were measured using infrared (IR) thermography. Roughness panels were CNC machined from plates of aluminum 6061 to create near isothermal roughness elements when heated. Fluid resistance differences between the aluminum roughness panels and roughness panels constructed from ABS plastic using the same roughness patterns from McClain et al. (2020, “Flow in a Simulated Turbine Blade Cooling Channel With Spatially Varying Roughness Caused by Additive Manufacturing Orientation,” ASME Turbo Expo 2020, Turbomachinery Technical Conference and Exposition, Virtual Conference, Sept. 21–25, GT2020-16069) were investigated. Finally, the overall thermal performance enhancements and friction losses were assessed through the calculation of surface averaged “global thermal performance” ratios. The global thermal performance characterizations indicate results in-line with those found for traditional commercial roughness and slightly below traditional internal passage convection enhancement methods such as swirl chambers, dimples, and ribs. The passages investigated in this study do not include compressibility effects or the long-wavelength artifacts and channel geometric deviations observed by Wildgoose et al. (2020, “Impact of Additive Manufacturing on Internal Cooling Channels with Varying Diameters and Build Directions,” ASME Turbo Expo 2020, Turbomachinery Technical Conference and Exposition, Virtual Conference, Sept. 21–25, GT2020-15049). However, the results of this study indicate that, based on the roughness augmentation alone, artificial convective cooling enhancers such as turbulators or dimples may still be required for additively manufactured turbine component cooling.
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      Convection in Scaled Turbine Internal Cooling Passages With Additive Manufacturing Roughness

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    contributor authorStafford, Gabriel J.
    contributor authorMcClain, Stephen T.
    contributor authorHanson, David R.
    contributor authorKunz, Robert F.
    contributor authorThole, Karen A.
    date accessioned2022-05-08T08:54:47Z
    date available2022-05-08T08:54:47Z
    date copyright11/10/2021 12:00:00 AM
    date issued2021
    identifier issn0889-504X
    identifier otherturbo_144_4_041008.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284501
    description abstractAdditive manufacturing processes, such as direct metal laser sintering (DMLS), enable the creation of novel turbine cooling internal passages and systems. However, the DMLS method produces a significant and unique surface roughness. Previous work in scaled passages analyzed pressure losses and friction factors associated with the rough surfaces, as well as investigated the velocity profiles and turbulent flow characteristics within the passage. In this study, the heat transfer characteristics of scaled additively manufactured surfaces were measured using infrared (IR) thermography. Roughness panels were CNC machined from plates of aluminum 6061 to create near isothermal roughness elements when heated. Fluid resistance differences between the aluminum roughness panels and roughness panels constructed from ABS plastic using the same roughness patterns from McClain et al. (2020, “Flow in a Simulated Turbine Blade Cooling Channel With Spatially Varying Roughness Caused by Additive Manufacturing Orientation,” ASME Turbo Expo 2020, Turbomachinery Technical Conference and Exposition, Virtual Conference, Sept. 21–25, GT2020-16069) were investigated. Finally, the overall thermal performance enhancements and friction losses were assessed through the calculation of surface averaged “global thermal performance” ratios. The global thermal performance characterizations indicate results in-line with those found for traditional commercial roughness and slightly below traditional internal passage convection enhancement methods such as swirl chambers, dimples, and ribs. The passages investigated in this study do not include compressibility effects or the long-wavelength artifacts and channel geometric deviations observed by Wildgoose et al. (2020, “Impact of Additive Manufacturing on Internal Cooling Channels with Varying Diameters and Build Directions,” ASME Turbo Expo 2020, Turbomachinery Technical Conference and Exposition, Virtual Conference, Sept. 21–25, GT2020-15049). However, the results of this study indicate that, based on the roughness augmentation alone, artificial convective cooling enhancers such as turbulators or dimples may still be required for additively manufactured turbine component cooling.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleConvection in Scaled Turbine Internal Cooling Passages With Additive Manufacturing Roughness
    typeJournal Paper
    journal volume144
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4052524
    journal fristpage41008-1
    journal lastpage41008-11
    page11
    treeJournal of Turbomachinery:;2021:;volume( 144 ):;issue: 004
    contenttypeFulltext
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