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    Analysis of NOX Formation in an Axially Staged Combustion System at Elevated Pressure Conditions

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 003::page 31507
    Author:
    Chockalingam Prathap
    ,
    Christian Beck
    ,
    Werner Krebs
    ,
    Flavio C. C. Galeazzo
    ,
    Plamen Kasabov
    ,
    Bernhard Wegner
    ,
    Peter Habisreuther
    ,
    Nikolaos Zarzalis
    DOI: 10.1115/1.4004720
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of this investigation was to study the effect of axially staged injection of methane in the vitiated air cross flow in a two stage combustion chamber on the formation of NOX for different momentum flux ratios. The primary cylindrical combustor equipped with a low swirl air blast nozzle operating with Jet-A liquid fuel generates vitiated air in the temperature range of 1473–1673 K at pressures of 5–8 bars. A methane injector was flush mounted to the inner surface of the secondary combustor at an angle of 30 deg. Oil cooled movable and static gas probes were used to collect the gas samples. The mole fractions of NO, NO2 , CO, CO2 , and O2 in the collected exhaust gas samples were measured using gas analyzers. For all the investigated operating conditions, the change in the mole fraction of NOX due to the injection of methane (ΔNOX ) corrected to 15% O2 and measured in dry mode was less than 15 ppm. The mole fraction of ΔNOX increased with an increase in mass flow rate of methane and it was not affected by a change in the momentum flux ratio. The penetration depth of the methane jet was estimated from the profiles of mole fraction of O2 obtained from the samples collected using the movable gas probe. For the investigated momentum flux ratios, the penetration depth observed was 15 mm at 5 bars and 5 mm at 6.5 and 8 bars. The results obtained from the simulations of the secondary combustor using a RANS turbulence model were also presented. Reaction modeling of the jet flame present in a vitiated air cross flow posed a significant challenge as it was embedded in a high turbulent flow and burns in partial premixed mode. The applicability of two different reaction models has been investigated. The first approach employed a combination of the eddy dissipation and the finite rate chemistry models to determine the reaction rate, while the presumed JPDF model was used in the further investigations. Predictions were in closer agreement to the measurements while employing the presumed JPDF model. This model was also able to predict some key features of the flow such as the change of penetration depth with the pressure.
    keyword(s): Pressure , Momentum , Flow (Dynamics) , Temperature , Combustion , Turbulence , Combustion chambers , Nozzles , Flames , Methane , Probes , Emissions , Fuels , Ejectors , Measurement , Cross-flow , Combustion systems , Modeling , Electrical discharge machining AND Engineering simulation ,
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      Analysis of NOX Formation in an Axially Staged Combustion System at Elevated Pressure Conditions

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/148892
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorChockalingam Prathap
    contributor authorChristian Beck
    contributor authorWerner Krebs
    contributor authorFlavio C. C. Galeazzo
    contributor authorPlamen Kasabov
    contributor authorBernhard Wegner
    contributor authorPeter Habisreuther
    contributor authorNikolaos Zarzalis
    date accessioned2017-05-09T00:50:30Z
    date available2017-05-09T00:50:30Z
    date copyrightMarch, 2012
    date issued2012
    identifier issn1528-8919
    identifier otherJETPEZ-27186#031507_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148892
    description abstractThe objective of this investigation was to study the effect of axially staged injection of methane in the vitiated air cross flow in a two stage combustion chamber on the formation of NOX for different momentum flux ratios. The primary cylindrical combustor equipped with a low swirl air blast nozzle operating with Jet-A liquid fuel generates vitiated air in the temperature range of 1473–1673 K at pressures of 5–8 bars. A methane injector was flush mounted to the inner surface of the secondary combustor at an angle of 30 deg. Oil cooled movable and static gas probes were used to collect the gas samples. The mole fractions of NO, NO2 , CO, CO2 , and O2 in the collected exhaust gas samples were measured using gas analyzers. For all the investigated operating conditions, the change in the mole fraction of NOX due to the injection of methane (ΔNOX ) corrected to 15% O2 and measured in dry mode was less than 15 ppm. The mole fraction of ΔNOX increased with an increase in mass flow rate of methane and it was not affected by a change in the momentum flux ratio. The penetration depth of the methane jet was estimated from the profiles of mole fraction of O2 obtained from the samples collected using the movable gas probe. For the investigated momentum flux ratios, the penetration depth observed was 15 mm at 5 bars and 5 mm at 6.5 and 8 bars. The results obtained from the simulations of the secondary combustor using a RANS turbulence model were also presented. Reaction modeling of the jet flame present in a vitiated air cross flow posed a significant challenge as it was embedded in a high turbulent flow and burns in partial premixed mode. The applicability of two different reaction models has been investigated. The first approach employed a combination of the eddy dissipation and the finite rate chemistry models to determine the reaction rate, while the presumed JPDF model was used in the further investigations. Predictions were in closer agreement to the measurements while employing the presumed JPDF model. This model was also able to predict some key features of the flow such as the change of penetration depth with the pressure.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of NOX Formation in an Axially Staged Combustion System at Elevated Pressure Conditions
    typeJournal Paper
    journal volume134
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4004720
    journal fristpage31507
    identifier eissn0742-4795
    keywordsPressure
    keywordsMomentum
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsCombustion
    keywordsTurbulence
    keywordsCombustion chambers
    keywordsNozzles
    keywordsFlames
    keywordsMethane
    keywordsProbes
    keywordsEmissions
    keywordsFuels
    keywordsEjectors
    keywordsMeasurement
    keywordsCross-flow
    keywordsCombustion systems
    keywordsModeling
    keywordsElectrical discharge machining AND Engineering simulation
    treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 003
    contenttypeFulltext
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