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    Optical Diagnostics of Late-Injection Low-Temperature Combustion in a Heavy-Duty Diesel Engine

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 003::page 32808
    Author:
    Thierry Lachaux
    ,
    Satbir Singh
    ,
    Rolf D. Reitz
    ,
    Mark P. Musculus
    DOI: 10.1115/1.2830864
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A late-injection, high exhaust-gas recirculation rate, low-temperature combustion strategy is investigated in a heavy-duty diesel engine using a suite of optical diagnostics: chemiluminescence for visualization of ignition and combustion, laser Mie scattering for liquid-fuel imaging, planar laser-induced fluorescence (PLIF) for both OH and vapor-fuel imagings, and laser-induced incandescence for soot imaging. Fuel is injected at top dead center when the in-cylinder gases are hot and dense. Consequently, the maximum liquid-fuel penetration is 27 mm, which is short enough to avoid wall impingement. The cool flame starts 4.5 crank angle degrees (CAD) after the start of injection (ASI), midway between the injector and bowl rim, and likely helps fuel to vaporize. Within a few CAD, the cool-flame combustion reaches the bowl rim. A large premixed combustion occurs near 9 CAD ASI, close to the bowl rim. Soot is visible shortly afterward, along the walls, typically between two adjacent jets. OH PLIF indicates that premixed combustion first occurs within the jet and then spreads along the bowl rim in a thin layer, surrounding soot pockets at the start of the mixing-controlled combustion phase near 17 CAD ASI. During the mixing-controlled phase, soot is not fully oxidized and is still present near the bowl rim late in the cycle. At the end of combustion near 27 CAD ASI, averaged PLIF images indicate two separate zones. OH PLIF appears near the bowl rim, while broadband PLIF persists late in the cycle near the injector. The most likely source of broadband PLIF is unburned fuel, which indicates that the near-injector region is a potential source of unburned hydrocarbons.
    keyword(s): Combustion , Fuels , Computer-aided design , Ejectors , Soot , Diesel engines , Lasers , Flames , Engines , Cylinders , Low temperature , Fluorescence , Chemiluminescence , Signals AND Diesel ,
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      Optical Diagnostics of Late-Injection Low-Temperature Combustion in a Heavy-Duty Diesel Engine

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    https://yetl.yabesh.ir/yetl1/handle/yetl/137950
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorThierry Lachaux
    contributor authorSatbir Singh
    contributor authorRolf D. Reitz
    contributor authorMark P. Musculus
    date accessioned2017-05-09T00:27:56Z
    date available2017-05-09T00:27:56Z
    date copyrightMay, 2008
    date issued2008
    identifier issn1528-8919
    identifier otherJETPEZ-27012#032808_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137950
    description abstractA late-injection, high exhaust-gas recirculation rate, low-temperature combustion strategy is investigated in a heavy-duty diesel engine using a suite of optical diagnostics: chemiluminescence for visualization of ignition and combustion, laser Mie scattering for liquid-fuel imaging, planar laser-induced fluorescence (PLIF) for both OH and vapor-fuel imagings, and laser-induced incandescence for soot imaging. Fuel is injected at top dead center when the in-cylinder gases are hot and dense. Consequently, the maximum liquid-fuel penetration is 27 mm, which is short enough to avoid wall impingement. The cool flame starts 4.5 crank angle degrees (CAD) after the start of injection (ASI), midway between the injector and bowl rim, and likely helps fuel to vaporize. Within a few CAD, the cool-flame combustion reaches the bowl rim. A large premixed combustion occurs near 9 CAD ASI, close to the bowl rim. Soot is visible shortly afterward, along the walls, typically between two adjacent jets. OH PLIF indicates that premixed combustion first occurs within the jet and then spreads along the bowl rim in a thin layer, surrounding soot pockets at the start of the mixing-controlled combustion phase near 17 CAD ASI. During the mixing-controlled phase, soot is not fully oxidized and is still present near the bowl rim late in the cycle. At the end of combustion near 27 CAD ASI, averaged PLIF images indicate two separate zones. OH PLIF appears near the bowl rim, while broadband PLIF persists late in the cycle near the injector. The most likely source of broadband PLIF is unburned fuel, which indicates that the near-injector region is a potential source of unburned hydrocarbons.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptical Diagnostics of Late-Injection Low-Temperature Combustion in a Heavy-Duty Diesel Engine
    typeJournal Paper
    journal volume130
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2830864
    journal fristpage32808
    identifier eissn0742-4795
    keywordsCombustion
    keywordsFuels
    keywordsComputer-aided design
    keywordsEjectors
    keywordsSoot
    keywordsDiesel engines
    keywordsLasers
    keywordsFlames
    keywordsEngines
    keywordsCylinders
    keywordsLow temperature
    keywordsFluorescence
    keywordsChemiluminescence
    keywordsSignals AND Diesel
    treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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