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    Low NOx Advanced Vortex Combustor

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 003::page 34502
    Author:
    Ryan G. Edmonds
    ,
    Robert C. Steele
    ,
    Douglas L. Straub
    ,
    Avtar Bining
    ,
    Kent H. Casleton
    ,
    Joseph T. Williams
    DOI: 10.1115/1.2838992
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A lean-premixed advanced vortex combustor (AVC) has been developed and tested. The natural gas fueled AVC was tested at the U.S. Department of Energy’s National Energy Technology Laboratory in Morgantown, WV. All testing was performed at elevated pressures and inlet temperatures and at lean fuel-air ratios representative of industrial gas turbines. The improved AVC design exhibited simultaneous NOx∕CO∕unburned hydrocarbon (UHC) emissions of 4∕4∕0ppmv (all emissions corrected to 15% O2 dry). The design also achieved less than 3ppmvNOx with combustion efficiencies in excess of 99.5%. The design demonstrated marked acoustic dynamic stability over a wide range of operating conditions, which potentially makes this approach significantly more attractive than other lean-premixed combustion approaches. In addition, the measured 1.75% pressure drop is significantly lower than conventional gas turbine combustors, which could translate into an overall gas turbine cycle efficiency improvement. The relatively high velocities and low pressure drop achievable with this technology make the AVC approach an attractive alternative for syngas fuel applications.
    keyword(s): Combustion , Fuels , Combustion chambers , Cavities , Emissions , Pressure drop , Vortices AND Dynamic stability ,
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      Low NOx Advanced Vortex Combustor

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/137958
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorRyan G. Edmonds
    contributor authorRobert C. Steele
    contributor authorDouglas L. Straub
    contributor authorAvtar Bining
    contributor authorKent H. Casleton
    contributor authorJoseph T. Williams
    date accessioned2017-05-09T00:27:56Z
    date available2017-05-09T00:27:56Z
    date copyrightMay, 2008
    date issued2008
    identifier issn1528-8919
    identifier otherJETPEZ-27012#034502_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137958
    description abstractA lean-premixed advanced vortex combustor (AVC) has been developed and tested. The natural gas fueled AVC was tested at the U.S. Department of Energy’s National Energy Technology Laboratory in Morgantown, WV. All testing was performed at elevated pressures and inlet temperatures and at lean fuel-air ratios representative of industrial gas turbines. The improved AVC design exhibited simultaneous NOx∕CO∕unburned hydrocarbon (UHC) emissions of 4∕4∕0ppmv (all emissions corrected to 15% O2 dry). The design also achieved less than 3ppmvNOx with combustion efficiencies in excess of 99.5%. The design demonstrated marked acoustic dynamic stability over a wide range of operating conditions, which potentially makes this approach significantly more attractive than other lean-premixed combustion approaches. In addition, the measured 1.75% pressure drop is significantly lower than conventional gas turbine combustors, which could translate into an overall gas turbine cycle efficiency improvement. The relatively high velocities and low pressure drop achievable with this technology make the AVC approach an attractive alternative for syngas fuel applications.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLow NOx Advanced Vortex Combustor
    typeJournal Paper
    journal volume130
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2838992
    journal fristpage34502
    identifier eissn0742-4795
    keywordsCombustion
    keywordsFuels
    keywordsCombustion chambers
    keywordsCavities
    keywordsEmissions
    keywordsPressure drop
    keywordsVortices AND Dynamic stability
    treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 003
    contenttypeFulltext
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