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    Experimental Investigation of Plasma Jet Ignition Characteristics in Kerosene–Air Mixtures

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 002
    Author:
    Bing-bing Zhao
    ,
    Gao-Cheng Chen
    ,
    Li-Ming He
    ,
    Tao Jin
    ,
    Bo Jing
    DOI: 10.1061/(ASCE)AS.1943-5525.0001108
    Publisher: ASCE
    Abstract: Ignition and high altitude restarts under extreme conditions have always been key research problems due to low pressure and temperature of inlet air, so reliable ignition and wide ignition boundary is very necessary. In this study, the ignition characteristics of kerosene/air mixtures at different excess air coefficients with a plasma jet ignition and spark ignition were investigated experimentally in a model combustor. The plasma ignition system utilizes compressed air as plasma formation gas. The spontaneous emissions of O atoms (777 nm) and CH radicals (430 nm) were collected by photomultiplier tubes with corresponding filters to identify the ignition and combustion timing during the ignition process. A plasma jet can penetrate a recirculation zone and initiate flame kernel, and the larger plasma volume and the activated area is very helpful to achieve successful ignition. The results show that a plasma jet ignition delay time is much shorter than that for spark ignition in a wide range of excess air coefficients; the minimum plasma jet ignition delay time can be reduced by 88.74% compared to spark ignition in the same experimental conditions. With the increase in plasma arc current, the ignition delay time can be further reduced.
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      Experimental Investigation of Plasma Jet Ignition Characteristics in Kerosene–Air Mixtures

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4266417
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    contributor authorBing-bing Zhao
    contributor authorGao-Cheng Chen
    contributor authorLi-Ming He
    contributor authorTao Jin
    contributor authorBo Jing
    date accessioned2022-01-30T20:02:37Z
    date available2022-01-30T20:02:37Z
    date issued2020
    identifier other%28ASCE%29AS.1943-5525.0001108.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4266417
    description abstractIgnition and high altitude restarts under extreme conditions have always been key research problems due to low pressure and temperature of inlet air, so reliable ignition and wide ignition boundary is very necessary. In this study, the ignition characteristics of kerosene/air mixtures at different excess air coefficients with a plasma jet ignition and spark ignition were investigated experimentally in a model combustor. The plasma ignition system utilizes compressed air as plasma formation gas. The spontaneous emissions of O atoms (777 nm) and CH radicals (430 nm) were collected by photomultiplier tubes with corresponding filters to identify the ignition and combustion timing during the ignition process. A plasma jet can penetrate a recirculation zone and initiate flame kernel, and the larger plasma volume and the activated area is very helpful to achieve successful ignition. The results show that a plasma jet ignition delay time is much shorter than that for spark ignition in a wide range of excess air coefficients; the minimum plasma jet ignition delay time can be reduced by 88.74% compared to spark ignition in the same experimental conditions. With the increase in plasma arc current, the ignition delay time can be further reduced.
    publisherASCE
    titleExperimental Investigation of Plasma Jet Ignition Characteristics in Kerosene–Air Mixtures
    typeJournal Paper
    journal volume33
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001108
    page04019113
    treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 002
    contenttypeFulltext
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