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contributor authorWang, Bo
contributor authorRosner, Fabian
contributor authorRao, Ashok
contributor authorZhao, Lifeng
contributor authorSamuelsen, Scott
date accessioned2022-02-06T05:30:44Z
date available2022-02-06T05:30:44Z
date copyright5/4/2021 12:00:00 AM
date issued2021
identifier issn0742-4795
identifier othergtp_143_09_094501.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278189
description abstractThe maximum firing temperature of a gas turbine (GT) is limited by material constraints. Critical for the operation of the GT is the blade metal temperature, which is impacted by the heat transfer from the combustor outlet gas to the blade surface. In this study, performance characteristics for an H-class-type GT have been established and two correlations for the change in the maximum permissible firing temperature as function of combustor outlet gas composition or flue gas composition and pressure ratio have been derived: (I) for detailed GT modeling with cooling flows and (II) for simplified GT modeling without specifying cooling flows.
publisherThe American Society of Mechanical Engineers (ASME)
titleMethod for Determining the Change in Gas Turbine Firing Temperature
typeJournal Paper
journal volume143
journal issue9
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4050859
journal fristpage094501-1
journal lastpage094501-4
page4
treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 009
contenttypeFulltext


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