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    Self-Adaptive Stability-Enhancing Technology With Tip Air Injection in an Axial Flow Compressor

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 001::page 11008
    Author:
    Li, Jichao
    DOI: 10.1115/1.4034553
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Self-adaptive stability control with discrete tip air injection and online detection of prestall inception is experimentally studied in a low-speed axial flow compressor. The control strategy is to sense the cross-correlation coefficient of the wall static pressure patterns and to feed back the signal to an annular array of eight separately proportional injecting valves. The real-time detecting algorithm based on cross-correlation theory is proposed and experimentally conducted using the axisymmetric arrangement of time-resolved sensors. Subsequently, the sensitivity of the cross-correlation coefficient to the discrete tip air injection is investigated. Thus, the control law is formed on the basis of the cross-correlation as a function of the injected momentum ratios. The steady injection and the on–off pulsating injection are simultaneously selected for comparison. Results show that the proposed self-adaptive stability control using digital signal processing (DSP) controller can save energy when the compressor is stable. This control also provides protection when needed. With nearly the same stall margin improvement (SMI) as the steady injection (maximum SMI is 44.2%), the energy of the injected air is roughly a quarter of the steady injection. Unlike the on–off pulsating jet, the new actuating scheme can reduce the unsteady force impinging onto the compressor blades caused by the pulsating jets in addition to achieve the much larger stability range extension.
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      Self-Adaptive Stability-Enhancing Technology With Tip Air Injection in an Axial Flow Compressor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4236009
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    contributor authorLi, Jichao
    date accessioned2017-11-25T07:19:47Z
    date available2017-11-25T07:19:47Z
    date copyright2016/20/9
    date issued2017
    identifier issn0889-504X
    identifier otherturbo_139_01_011008.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4236009
    description abstractSelf-adaptive stability control with discrete tip air injection and online detection of prestall inception is experimentally studied in a low-speed axial flow compressor. The control strategy is to sense the cross-correlation coefficient of the wall static pressure patterns and to feed back the signal to an annular array of eight separately proportional injecting valves. The real-time detecting algorithm based on cross-correlation theory is proposed and experimentally conducted using the axisymmetric arrangement of time-resolved sensors. Subsequently, the sensitivity of the cross-correlation coefficient to the discrete tip air injection is investigated. Thus, the control law is formed on the basis of the cross-correlation as a function of the injected momentum ratios. The steady injection and the on–off pulsating injection are simultaneously selected for comparison. Results show that the proposed self-adaptive stability control using digital signal processing (DSP) controller can save energy when the compressor is stable. This control also provides protection when needed. With nearly the same stall margin improvement (SMI) as the steady injection (maximum SMI is 44.2%), the energy of the injected air is roughly a quarter of the steady injection. Unlike the on–off pulsating jet, the new actuating scheme can reduce the unsteady force impinging onto the compressor blades caused by the pulsating jets in addition to achieve the much larger stability range extension.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSelf-Adaptive Stability-Enhancing Technology With Tip Air Injection in an Axial Flow Compressor
    typeJournal Paper
    journal volume139
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4034553
    journal fristpage11008
    journal lastpage011008-9
    treeJournal of Turbomachinery:;2017:;volume( 139 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian