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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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