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contributor authorAx, Holger
contributor authorLammel, Oliver
contributor authorLückerath, Rainer
contributor authorSeverin, Michael
date accessioned2022-02-04T22:00:04Z
date available2022-02-04T22:00:04Z
date copyright7/1/2020 12:00:00 AM
date issued2020
identifier issn0742-4795
identifier othergtp_142_07_071011.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4274680
description abstractA detailed investigation on flame structures and stabilization mechanisms of confined high momentum jet flames by one-dimensional (1D)-laser Raman measurements is presented. The flames were operated with natural gas (NG) at gas turbine relevant conditions in an optically accessible high-pressure test rig. The generic burner represents a full scale single nozzle of a high temperature FLOX® gas turbine combustor including a pilot stage. 1D-laser Raman measurements were performed on both an unpiloted and a piloted flame and evaluated on a single shot basis revealing the thermochemical states from unburned inflow conditions to burned hot gas in terms of average and statistical values of the major species concentrations, the mixture fraction and the temperature. The results show a distinct difference in the flame stabilization mechanism between the unpiloted and the piloted case. The former is apparently driven by strong mixing of fresh unburned gas and recirculated hot burned gas that eventually causes autoignition. The piloted flame is stabilized by the pilot stage followed by turbulent flame propagation. The findings help to understand the underlying combustion mechanisms and to further develop gas turbine burners following the FLOX concept.
publisherThe American Society of Mechanical Engineers (ASME)
titleHigh-Momentum Jet Flames at Elevated Pressure, C: Statistical Distribution of Thermochemical States Obtained From Laser-Raman Measurements
typeJournal Paper
journal volume142
journal issue7
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4045483
journal fristpage071011-1
journal lastpage071011-8
page8
treeJournal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 007
contenttypeFulltext


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