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    Wall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry

    Source: Journal of Turbomachinery:;2020:;volume( 143 ):;issue: 001::page 011007-1
    Author:
    Nau, Patrick
    ,
    Görs, Simon
    ,
    Arndt, Christoph
    ,
    Witzel, Benjamin
    ,
    Endres, Torsten
    DOI: 10.1115/1.4049104
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Wall temperature measurements with fiber coupled online phosphor thermometry were, for the first time, successfully performed in a full-scale H-class Siemens gas turbine combustor. Online wall temperatures were obtained during high-pressure combustion tests up to 8 bar at the Siemens Clean Energy Center (CEC) test facility. Since optical access to the combustion chamber with fibers being able to provide high laser energies is extremely challenging, we developed a custom-built measurement system consisting of a water-cooled fiber optic probe and a mobile measurement container. A suitable combination of chemical binder and thermographic phosphor was identified for temperatures up to 1800 K on combustor walls coated with a thermal barrier coating (TBC). To our knowledge, these are the first measurements reported with fiber coupled online phosphor thermometry in a full-scale high-pressure gas turbine combustor. Details of the setup and the measurement procedures will be presented. The measured signals were influenced by strong background emissions probably from CO*2 chemiluminescence. Strategies for correcting background emissions and data evaluation procedures are discussed. The presented measurement technique enables the detailed study of combustor wall temperatures and using this information an optimization of the gas turbine cooling design.
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      Wall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4276943
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    contributor authorNau, Patrick
    contributor authorGörs, Simon
    contributor authorArndt, Christoph
    contributor authorWitzel, Benjamin
    contributor authorEndres, Torsten
    date accessioned2022-02-05T22:06:57Z
    date available2022-02-05T22:06:57Z
    date copyright12/28/2020 12:00:00 AM
    date issued2020
    identifier issn0889-504X
    identifier otherturbo_143_1_011007.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4276943
    description abstractWall temperature measurements with fiber coupled online phosphor thermometry were, for the first time, successfully performed in a full-scale H-class Siemens gas turbine combustor. Online wall temperatures were obtained during high-pressure combustion tests up to 8 bar at the Siemens Clean Energy Center (CEC) test facility. Since optical access to the combustion chamber with fibers being able to provide high laser energies is extremely challenging, we developed a custom-built measurement system consisting of a water-cooled fiber optic probe and a mobile measurement container. A suitable combination of chemical binder and thermographic phosphor was identified for temperatures up to 1800 K on combustor walls coated with a thermal barrier coating (TBC). To our knowledge, these are the first measurements reported with fiber coupled online phosphor thermometry in a full-scale high-pressure gas turbine combustor. Details of the setup and the measurement procedures will be presented. The measured signals were influenced by strong background emissions probably from CO*2 chemiluminescence. Strategies for correcting background emissions and data evaluation procedures are discussed. The presented measurement technique enables the detailed study of combustor wall temperatures and using this information an optimization of the gas turbine cooling design.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleWall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry
    typeJournal Paper
    journal volume143
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4049104
    journal fristpage011007-1
    journal lastpage011007-7
    page7
    treeJournal of Turbomachinery:;2020:;volume( 143 ):;issue: 001
    contenttypeFulltext
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