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    Passive Suppression of Self-Excited Combustion Instabilities in Liquid Spray Flame Using Microperforated Plate

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 011::page 0111013-1
    Author:
    Zhou, Hao
    ,
    Liu, Zihua
    ,
    Tao, Chengfei
    ,
    Zhou, Mingxi
    DOI: 10.1115/1.4047768
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an experimental investigation of using a microperforated plate (MPP) backed by an adjustable cavity to mitigate the combustion instabilities of liquid fuel swirl flame. The acoustic properties of MPPs with different porosities and aperture diameters were first tested in an impedance tube. At low bias flow rates, the sound reflection coefficients of MPPs with large holes commensurate well with the Luong model, and at high bias flow rates, the results of MPPs with small holes agree well with the predictions. The maximum sound absorption coefficient of each panel at the target frequency exceeded 95%. The perforated panels were then selected and integrated into a spray combustor individually. It was shown that the maximum reduction of pressure and heat release fluctuations inside the chamber was 14.91 dB and 13.40 dB, respectively. After noise elimination, the main frequencies of pressure and CH* signals were slightly shifted toward low frequencies. When the combustion conditions change, the MPPs operating near the optimal bias flow rates still have good sound absorption characteristics. After noise suppression, the synchronization between pressure and heat release signals was reduced, and the flame shapes were relatively stable. More generally, this study can promote the application of MPPs under bias flow in stabilizing the liquid spray combustion.
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      Passive Suppression of Self-Excited Combustion Instabilities in Liquid Spray Flame Using Microperforated Plate

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4274693
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    contributor authorZhou, Hao
    contributor authorLiu, Zihua
    contributor authorTao, Chengfei
    contributor authorZhou, Mingxi
    date accessioned2022-02-04T22:00:22Z
    date available2022-02-04T22:00:22Z
    date copyright10/29/2020 12:00:00 AM
    date issued2020
    identifier issn0742-4795
    identifier othergtp_142_08_085001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4274693
    description abstractThis paper presents an experimental investigation of using a microperforated plate (MPP) backed by an adjustable cavity to mitigate the combustion instabilities of liquid fuel swirl flame. The acoustic properties of MPPs with different porosities and aperture diameters were first tested in an impedance tube. At low bias flow rates, the sound reflection coefficients of MPPs with large holes commensurate well with the Luong model, and at high bias flow rates, the results of MPPs with small holes agree well with the predictions. The maximum sound absorption coefficient of each panel at the target frequency exceeded 95%. The perforated panels were then selected and integrated into a spray combustor individually. It was shown that the maximum reduction of pressure and heat release fluctuations inside the chamber was 14.91 dB and 13.40 dB, respectively. After noise elimination, the main frequencies of pressure and CH* signals were slightly shifted toward low frequencies. When the combustion conditions change, the MPPs operating near the optimal bias flow rates still have good sound absorption characteristics. After noise suppression, the synchronization between pressure and heat release signals was reduced, and the flame shapes were relatively stable. More generally, this study can promote the application of MPPs under bias flow in stabilizing the liquid spray combustion.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePassive Suppression of Self-Excited Combustion Instabilities in Liquid Spray Flame Using Microperforated Plate
    typeJournal Paper
    journal volume142
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4047768
    journal fristpage0111013-1
    journal lastpage0111013-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 011
    contenttypeFulltext
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