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    Ignition Delay and Combustion Characteristics of Gaseous Fuel Jets

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 004::page 42804
    Author:
    Dung Ngoc Nguyen
    ,
    Hiroaki Ishida
    ,
    Masahiro Shioji
    DOI: 10.1115/1.4000115
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gaseous fuels, such as hydrogen and natural gas, are utilized in internal combustion engines for spark-ignition operation. To improve thermal efficiency and to ensure control at good heat-release rates, combustion systems with direct-injection and spontaneous-ignition operation may be preferable. The main objective of this research was to provide fundamental data for the ignition and combustion of hydrogen, natural gas, and methane. Experiments were conducted in a constant-volume combustion vessel to investigate the effects of ambient temperature on ignition delay and combustion characteristics for various injector and ambient conditions. Experimental results showed that all gaseous fuels exhibited similar ignition-delay trends: ignition delay (τ) increased as ambient temperature (Ti) decreased. Among these fuels, hydrogen jets exhibited much shorter τ than natural gas and methane jets at the same Ti and could be ignited at a lower temperature, Ti=780 K. A shorter ignition delay of hydrogen may be attained by controlling the mixture formation by lowering the injection pressure (pj), enlarging the nozzle-hole diameter (dN), increasing the ambient pressure (pi), and increasing the oxygen mole fraction (rO2). In contrast, the methane jet exhibited the longest τ over the whole range of Ti and suffered from misfiring at a higher Ti of 910 K. For natural gas, ignition delay was observed to be shorter than that for methane, owing to a small amount of butane with good ignitability. More specifically, the ignition delay of natural gas differed slightly when dN and pj varied but changed drastically when pi and rO2 decreased. Based on these data, the feasibility of gaseous fuels for compression-ignition engines is discussed from the viewpoint of mixture formation and chemical reaction.
    keyword(s): Pressure , Temperature , Combustion , Fuels , Jets , Natural gas , Delays , Hydrogen , Ignition , Mixtures AND Oxygen ,
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      Ignition Delay and Combustion Characteristics of Gaseous Fuel Jets

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    https://yetl.yabesh.ir/yetl1/handle/yetl/143237
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorDung Ngoc Nguyen
    contributor authorHiroaki Ishida
    contributor authorMasahiro Shioji
    date accessioned2017-05-09T00:37:48Z
    date available2017-05-09T00:37:48Z
    date copyrightApril, 2010
    date issued2010
    identifier issn1528-8919
    identifier otherJETPEZ-27107#042804_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143237
    description abstractGaseous fuels, such as hydrogen and natural gas, are utilized in internal combustion engines for spark-ignition operation. To improve thermal efficiency and to ensure control at good heat-release rates, combustion systems with direct-injection and spontaneous-ignition operation may be preferable. The main objective of this research was to provide fundamental data for the ignition and combustion of hydrogen, natural gas, and methane. Experiments were conducted in a constant-volume combustion vessel to investigate the effects of ambient temperature on ignition delay and combustion characteristics for various injector and ambient conditions. Experimental results showed that all gaseous fuels exhibited similar ignition-delay trends: ignition delay (τ) increased as ambient temperature (Ti) decreased. Among these fuels, hydrogen jets exhibited much shorter τ than natural gas and methane jets at the same Ti and could be ignited at a lower temperature, Ti=780 K. A shorter ignition delay of hydrogen may be attained by controlling the mixture formation by lowering the injection pressure (pj), enlarging the nozzle-hole diameter (dN), increasing the ambient pressure (pi), and increasing the oxygen mole fraction (rO2). In contrast, the methane jet exhibited the longest τ over the whole range of Ti and suffered from misfiring at a higher Ti of 910 K. For natural gas, ignition delay was observed to be shorter than that for methane, owing to a small amount of butane with good ignitability. More specifically, the ignition delay of natural gas differed slightly when dN and pj varied but changed drastically when pi and rO2 decreased. Based on these data, the feasibility of gaseous fuels for compression-ignition engines is discussed from the viewpoint of mixture formation and chemical reaction.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleIgnition Delay and Combustion Characteristics of Gaseous Fuel Jets
    typeJournal Paper
    journal volume132
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4000115
    journal fristpage42804
    identifier eissn0742-4795
    keywordsPressure
    keywordsTemperature
    keywordsCombustion
    keywordsFuels
    keywordsJets
    keywordsNatural gas
    keywordsDelays
    keywordsHydrogen
    keywordsIgnition
    keywordsMixtures AND Oxygen
    treeJournal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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