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    Particulate Deposition Effects on Internal Swirl Cooling of Turbine Blades

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 145 ):;issue: 005::page 51020-1
    Author:
    Yang, Xing
    ,
    Hao, Zihan
    ,
    Seibold, Florian
    ,
    Feng, Zhenping
    ,
    Ligrani, Phillip
    ,
    Weigand, Bernhard
    DOI: 10.1115/1.4056264
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Particulate deposition effects on flow and heat transfer in an internal swirl tube subjected to fly ash ingestion were investigated by constructing an unsteady simulation framework, in which a particle–wall interaction model and a mesh morphing technique were implemented. Swirling flows in the swirl tube were induced by two tangential jet nozzles. Particles having a mean diameter of 6.5 μm were released from the nozzle inlets to model an exposure duration of 4500 h for engine operation in real fly ash environment using scale factors in the unsteady simulations. Particle deposition and its dynamic process were examined, and the effects of deposition on the swirling flow were quantified by comparing time-averaged velocity profiles, vorticity, pressure loss, and heat transfer with those from a clean tube without deposition. Results reveal that the most upstream section of the swirl tube captures the majority of the particles and the deposition distributions show a spiral pattern over the tube wall. The total mass of the deposits within the tube linearly increases, while local deposition thickness has a nonlinear relationship with the exposure time due to the interaction of the particles with the swirling flow. The deposition can generate a maximum of 15% reduction in cross-sectional area of the tube within the exposure duration, resulting in a reduced swirl number, because of the accelerated axial velocity and the decreased circumferential velocity, and further lower heat transfer in the downstream section of the tube relative to the clean tube case. However, as the heat transfer in the upstream deposition section is enhanced by the roughness due to the deposition, area-averaged heat transfer throughout the entire swirl tube is slightly improved by 4.0% but simultaneously a 179% higher pressure loss is observed, leading to an overall thermal performance value of 0.79 (relative to 1.0 for a clean tube), indicating substantial degradation of cooling performance in the fouled swirl tube.
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      Particulate Deposition Effects on Internal Swirl Cooling of Turbine Blades

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4291884
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    contributor authorYang, Xing
    contributor authorHao, Zihan
    contributor authorSeibold, Florian
    contributor authorFeng, Zhenping
    contributor authorLigrani, Phillip
    contributor authorWeigand, Bernhard
    date accessioned2023-08-16T18:22:53Z
    date available2023-08-16T18:22:53Z
    date copyright1/10/2023 12:00:00 AM
    date issued2023
    identifier issn0742-4795
    identifier othergtp_145_05_051020.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291884
    description abstractParticulate deposition effects on flow and heat transfer in an internal swirl tube subjected to fly ash ingestion were investigated by constructing an unsteady simulation framework, in which a particle–wall interaction model and a mesh morphing technique were implemented. Swirling flows in the swirl tube were induced by two tangential jet nozzles. Particles having a mean diameter of 6.5 μm were released from the nozzle inlets to model an exposure duration of 4500 h for engine operation in real fly ash environment using scale factors in the unsteady simulations. Particle deposition and its dynamic process were examined, and the effects of deposition on the swirling flow were quantified by comparing time-averaged velocity profiles, vorticity, pressure loss, and heat transfer with those from a clean tube without deposition. Results reveal that the most upstream section of the swirl tube captures the majority of the particles and the deposition distributions show a spiral pattern over the tube wall. The total mass of the deposits within the tube linearly increases, while local deposition thickness has a nonlinear relationship with the exposure time due to the interaction of the particles with the swirling flow. The deposition can generate a maximum of 15% reduction in cross-sectional area of the tube within the exposure duration, resulting in a reduced swirl number, because of the accelerated axial velocity and the decreased circumferential velocity, and further lower heat transfer in the downstream section of the tube relative to the clean tube case. However, as the heat transfer in the upstream deposition section is enhanced by the roughness due to the deposition, area-averaged heat transfer throughout the entire swirl tube is slightly improved by 4.0% but simultaneously a 179% higher pressure loss is observed, leading to an overall thermal performance value of 0.79 (relative to 1.0 for a clean tube), indicating substantial degradation of cooling performance in the fouled swirl tube.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleParticulate Deposition Effects on Internal Swirl Cooling of Turbine Blades
    typeJournal Paper
    journal volume145
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4056264
    journal fristpage51020-1
    journal lastpage51020-13
    page13
    treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 145 ):;issue: 005
    contenttypeFulltext
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