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    Monitoring of Aerodynamic Load and Detection of Stall in Multistage Axial Compressors

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001::page 81
    Author:
    H. Hönen
    ,
    H. E. Gallus
    DOI: 10.1115/1.2835645
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady flow in a single-stage axial flow compressor at different operating conditions has been investigated with hot-wire and hot-film probes to find out the influence of the aerodynamic compressor load on the periodic fluctuations. These results are compared with measurements in the last stages of a multistage high-pressure compressor of a gas turbine for normal operation and under stall conditions. From the patterns of the frequency spectra of the measuring signals a parameter for the detection of the approach to the stability line of a compressor is derived. A method for the on-line monitoring of the aerodynamic load is presented. Based on these results a monitoring system has been developed. First experiences with this system, applied to two multistage compressors, are reported.
    keyword(s): Stress , Compressors , Wire , Stability , Spectra (Spectroscopy) , Measurement , Fluctuations (Physics) , High pressure (Physics) , Gas turbines , Axial flow , Monitoring systems , Probes , Signals AND Unsteady flow ,
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      Monitoring of Aerodynamic Load and Detection of Stall in Multistage Axial Compressors

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/116173
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    • Journal of Turbomachinery

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    contributor authorH. Hönen
    contributor authorH. E. Gallus
    date accessioned2017-05-08T23:48:39Z
    date available2017-05-08T23:48:39Z
    date copyrightJanuary, 1995
    date issued1995
    identifier issn0889-504X
    identifier otherJOTUEI-28642#81_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116173
    description abstractThe unsteady flow in a single-stage axial flow compressor at different operating conditions has been investigated with hot-wire and hot-film probes to find out the influence of the aerodynamic compressor load on the periodic fluctuations. These results are compared with measurements in the last stages of a multistage high-pressure compressor of a gas turbine for normal operation and under stall conditions. From the patterns of the frequency spectra of the measuring signals a parameter for the detection of the approach to the stability line of a compressor is derived. A method for the on-line monitoring of the aerodynamic load is presented. Based on these results a monitoring system has been developed. First experiences with this system, applied to two multistage compressors, are reported.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMonitoring of Aerodynamic Load and Detection of Stall in Multistage Axial Compressors
    typeJournal Paper
    journal volume117
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2835645
    journal fristpage81
    journal lastpage86
    identifier eissn1528-8900
    keywordsStress
    keywordsCompressors
    keywordsWire
    keywordsStability
    keywordsSpectra (Spectroscopy)
    keywordsMeasurement
    keywordsFluctuations (Physics)
    keywordsHigh pressure (Physics)
    keywordsGas turbines
    keywordsAxial flow
    keywordsMonitoring systems
    keywordsProbes
    keywordsSignals AND Unsteady flow
    treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 001
    contenttypeFulltext
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    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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