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    Compressor Fault Identification From Overall Performance Data Based on Adaptive Stage Stacking

    Source: Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 001::page 156
    Author:
    K. Mathioudakis
    ,
    A. Stamatis
    DOI: 10.1115/1.2906785
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the present paper a method for the identification of faulty stages in a multistage compressor is presented. The values of overall compressor parameters, namely mass flow rate, pressure ratio, and efficiency, at different operating points are the input data to the method. Employing these data, the method gives the location and the number of faulty stages, as well as the amount of deviation from intact condition performance. It is shown that the kind of fault that has caused stage performance deterioration can be identified. Features of the method, such as generality of applicability, input data requirement, and reliability of the findings, are discussed.
    keyword(s): Compressors , Reliability , Pressure AND Flow (Dynamics) ,
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      Compressor Fault Identification From Overall Performance Data Based on Adaptive Stage Stacking

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/113621
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorK. Mathioudakis
    contributor authorA. Stamatis
    date accessioned2017-05-08T23:44:16Z
    date available2017-05-08T23:44:16Z
    date copyrightJanuary, 1994
    date issued1994
    identifier issn1528-8919
    identifier otherJETPEZ-26722#156_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113621
    description abstractIn the present paper a method for the identification of faulty stages in a multistage compressor is presented. The values of overall compressor parameters, namely mass flow rate, pressure ratio, and efficiency, at different operating points are the input data to the method. Employing these data, the method gives the location and the number of faulty stages, as well as the amount of deviation from intact condition performance. It is shown that the kind of fault that has caused stage performance deterioration can be identified. Features of the method, such as generality of applicability, input data requirement, and reliability of the findings, are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCompressor Fault Identification From Overall Performance Data Based on Adaptive Stage Stacking
    typeJournal Paper
    journal volume116
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906785
    journal fristpage156
    journal lastpage164
    identifier eissn0742-4795
    keywordsCompressors
    keywordsReliability
    keywordsPressure AND Flow (Dynamics)
    treeJournal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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