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    Emissions Performance of the Parker Macrolaminate Premixer Tested Under Simulated Engine Conditions

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 003::page 465
    Author:
    Adel Mansour
    ,
    Michael A. Benjamin
    DOI: 10.1115/1.1762907
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Single-injector high-pressure rig evaluation of the prototype Parker macrolaminate dual fuel premixer (previously tested at NETL, Mansour et al., 2001) with pressure swirl macrolaminate atomizers was conducted under simulated engine operating conditions running on No. 2 diesel fuel (DF2). Emissions, oscillations and lean blowout (LBO) performance on liquid fuel at high, part and no load operating points (pressures of 160, 100, 120 psig, and inlet temperatures of 690, 570, 590°F, respectively) and various pressure drops (ΔP/P) and air fuel ratio conditions were investigated. The results indicate that the Parker premixer design has the potential to reduce the DF2 NOX emission to below 15 ppmv, 15% O2. At simulated high load conditions with a nominal flame temperature (TPZ) of 2700°F, the NOX and CO emissions are approximately 10 and 2.5 ppmv at 15% O2, respectively. These NOX results have not been corrected for fuel bound nitrogen (FBN). From the studies of Lee (2000), small amounts of FBN in the liquid fuel generally are completely converted over to fuel NOX under lean premixed conditions. The fuel tested has a nominal 60 ppmw of FBN which converts to an estimated fuel NOX of 4 ppmv at 15% O2. These results compare extremely favorable to existing commercially available premixer technologies tested under similar rig operating conditions. More importantly, the NOX yield for the Parker Macrolaminate premixer appears to be independent of operating conditions (from high to no load and various pressure drop conditions). Variations in combustor pressure, inlet temperature (T2) and residence time (τ) or pressure drop (ΔP/P) does not seem to have an effect on the formation of NOX. According to Leonard and Stegmaier (1993), insensitivity of NOX formation to operating conditions is a good indication of high degree of premixing. Additionally, the premixer NOX data is only 1 to 2 ppmv higher than the jet stirred reactor (JSR) results (ran at T2=661°F,PCD=1 atm and TPZ=2762°F with similar DF2) of Lee et al. (2001) further confirming the quality of premixing achieved. Combustion driven oscillations was not investigated by tuning the rig so that oscillations would not be a factor.
    keyword(s): Pressure , Fuels , Engines , Combustion chambers , Emissions , Flames , Oscillations , Combustion , Design , Stress , Ejectors , Temperature AND Engineering prototypes ,
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      Emissions Performance of the Parker Macrolaminate Premixer Tested Under Simulated Engine Conditions

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    https://yetl.yabesh.ir/yetl1/handle/yetl/129992
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorAdel Mansour
    contributor authorMichael A. Benjamin
    date accessioned2017-05-09T00:12:57Z
    date available2017-05-09T00:12:57Z
    date copyrightJuly, 2004
    date issued2004
    identifier issn1528-8919
    identifier otherJETPEZ-26829#465_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129992
    description abstractSingle-injector high-pressure rig evaluation of the prototype Parker macrolaminate dual fuel premixer (previously tested at NETL, Mansour et al., 2001) with pressure swirl macrolaminate atomizers was conducted under simulated engine operating conditions running on No. 2 diesel fuel (DF2). Emissions, oscillations and lean blowout (LBO) performance on liquid fuel at high, part and no load operating points (pressures of 160, 100, 120 psig, and inlet temperatures of 690, 570, 590°F, respectively) and various pressure drops (ΔP/P) and air fuel ratio conditions were investigated. The results indicate that the Parker premixer design has the potential to reduce the DF2 NOX emission to below 15 ppmv, 15% O2. At simulated high load conditions with a nominal flame temperature (TPZ) of 2700°F, the NOX and CO emissions are approximately 10 and 2.5 ppmv at 15% O2, respectively. These NOX results have not been corrected for fuel bound nitrogen (FBN). From the studies of Lee (2000), small amounts of FBN in the liquid fuel generally are completely converted over to fuel NOX under lean premixed conditions. The fuel tested has a nominal 60 ppmw of FBN which converts to an estimated fuel NOX of 4 ppmv at 15% O2. These results compare extremely favorable to existing commercially available premixer technologies tested under similar rig operating conditions. More importantly, the NOX yield for the Parker Macrolaminate premixer appears to be independent of operating conditions (from high to no load and various pressure drop conditions). Variations in combustor pressure, inlet temperature (T2) and residence time (τ) or pressure drop (ΔP/P) does not seem to have an effect on the formation of NOX. According to Leonard and Stegmaier (1993), insensitivity of NOX formation to operating conditions is a good indication of high degree of premixing. Additionally, the premixer NOX data is only 1 to 2 ppmv higher than the jet stirred reactor (JSR) results (ran at T2=661°F,PCD=1 atm and TPZ=2762°F with similar DF2) of Lee et al. (2001) further confirming the quality of premixing achieved. Combustion driven oscillations was not investigated by tuning the rig so that oscillations would not be a factor.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEmissions Performance of the Parker Macrolaminate Premixer Tested Under Simulated Engine Conditions
    typeJournal Paper
    journal volume126
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1762907
    journal fristpage465
    journal lastpage471
    identifier eissn0742-4795
    keywordsPressure
    keywordsFuels
    keywordsEngines
    keywordsCombustion chambers
    keywordsEmissions
    keywordsFlames
    keywordsOscillations
    keywordsCombustion
    keywordsDesign
    keywordsStress
    keywordsEjectors
    keywordsTemperature AND Engineering prototypes
    treeJournal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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