1994
DOI: 10.1115/1.2906853
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Development of an Aeroderivative Gas Turbine Dry Low Emissions Combustion System

Abstract: This paper gives the development status of GE’s new aeroderivative premixed combustion system. This system consists of a new fuel staged annular combustor, compressor rear frame, first-stage turbine nozzle, electronic staging controller, and fuel delivery system. Component test results along with a description of the combustion system are presented. This new system will reduce NOx emissions by 90 percent relative to the original aircraft engine combustion system while maintaining low emissions of CO and UHCs. … Show more

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Cited by 95 publications
(42 citation statements)
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“…The basic GE design consists of concentric counter-swirling annular flows. The constraints and challenges in implementing these concepts is discussed in a series of papers and research reports published by GE [Davis and Black;Correa, 1992;Leonard and Stegmaier, 1993;Joshi et al, 1994].…”
Section: Modeling Of Gas Turbine Combustorsmentioning
confidence: 99%
See 3 more Smart Citations
“…The basic GE design consists of concentric counter-swirling annular flows. The constraints and challenges in implementing these concepts is discussed in a series of papers and research reports published by GE [Davis and Black;Correa, 1992;Leonard and Stegmaier, 1993;Joshi et al, 1994].…”
Section: Modeling Of Gas Turbine Combustorsmentioning
confidence: 99%
“…The following section provides the results of modeling NOx formation in premixed flames for the conditions of interest in gas turbines. Leonard and Stegmaier (1993) provide NOx measurements in a premixed isothermal plug-flow flame reported at 15%O 2 dry, shown in Figure I.1. The data were taken for premixed flames stabilized with a variety of flame holders, for pressures of 1 to 30 bar, inlet air temperatures of 300 to 800K, and residence times of 2 to 100 milliseconds.…”
Section: Modeling Of Gas Turbine Combustorsmentioning
confidence: 99%
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“…First of all, the fuel is injected and vaporized in a flow of hot air with which it mixes. In this zone, complete evaporation and a homogeneous mixture must be achieved before the reaction zone preferably just above the low extinction limit in order to limit the formation of NO x emissions (Leonard andStegmaïer, 1993, Ripplinger et al, 1998). The flame is then stabilized with the creation of re-circulation zones, and combustion proceeds with a maximum flame temperature generally lower than 2000K (Poeschl et al, 1994, Ohkubo et al, 1994.…”
Section: The Combustion Chambermentioning
confidence: 99%