YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Stall Precursor Identification in High-Speed Compressor Stages Using Chaotic Time Series Analysis Methods

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003::page 491
    Author:
    M. M. Bright
    ,
    H. K. Qammar
    ,
    H. J. Weigl
    ,
    J. D. Paduano
    DOI: 10.1115/1.2841148
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a new technique for precursor identification in high-speed compressors. The technique is a pseudo-correlation integral method referred to as the correlation method. To provide a basis for comparison, the traveling wave energy technique, which has been used extensively to study prestall data, is also briefly presented and applied. The correlation method has a potential advantage over the traveling wave energy method because it uses a single sensor for detection. It also requires no predisposition about the expected behavior of the data to detect “changes” in the behavior of the compressor. Both methods are used in this study to identify stall precursive events in the pressure fluctuations measured from circumferential pressure transducers located at the front face of the compressor rig. The correlation method successfully identified stall formation or changes in the compressor dynamics from data captured from four different configurations of a NASA Lewis single-stage high-speed compressor while it was transitioned from stable operation into stall. This paper includes an exposition on the use of nonlinear methods to identify stall precursors, a description of the methodologies used for the study, information on the NASA high-speed compressor rig and experimental data acquisition, and results from the four compressor configurations. The experimental results indicate that the correlation method provides ample warning of the onset of rotating stall at high speed, in some tests on the order of 2000 rotor revolutions. Complementary features of the correlation method and the traveling wave energy method are discussed, and suggestions for future developments are made.
    keyword(s): Compressors , Time series , Travel , Wave energy , Data acquisition , Pressure transducers , Fluctuations (Physics) , Rotors , Dynamics (Mechanics) , Pressure AND Sensors ,
    • Download: (1.055Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Stall Precursor Identification in High-Speed Compressor Stages Using Chaotic Time Series Analysis Methods

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/119596
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorM. M. Bright
    contributor authorH. K. Qammar
    contributor authorH. J. Weigl
    contributor authorJ. D. Paduano
    date accessioned2017-05-08T23:55:05Z
    date available2017-05-08T23:55:05Z
    date copyrightJuly, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28661#491_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119596
    description abstractThis paper presents a new technique for precursor identification in high-speed compressors. The technique is a pseudo-correlation integral method referred to as the correlation method. To provide a basis for comparison, the traveling wave energy technique, which has been used extensively to study prestall data, is also briefly presented and applied. The correlation method has a potential advantage over the traveling wave energy method because it uses a single sensor for detection. It also requires no predisposition about the expected behavior of the data to detect “changes” in the behavior of the compressor. Both methods are used in this study to identify stall precursive events in the pressure fluctuations measured from circumferential pressure transducers located at the front face of the compressor rig. The correlation method successfully identified stall formation or changes in the compressor dynamics from data captured from four different configurations of a NASA Lewis single-stage high-speed compressor while it was transitioned from stable operation into stall. This paper includes an exposition on the use of nonlinear methods to identify stall precursors, a description of the methodologies used for the study, information on the NASA high-speed compressor rig and experimental data acquisition, and results from the four compressor configurations. The experimental results indicate that the correlation method provides ample warning of the onset of rotating stall at high speed, in some tests on the order of 2000 rotor revolutions. Complementary features of the correlation method and the traveling wave energy method are discussed, and suggestions for future developments are made.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStall Precursor Identification in High-Speed Compressor Stages Using Chaotic Time Series Analysis Methods
    typeJournal Paper
    journal volume119
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841148
    journal fristpage491
    journal lastpage499
    identifier eissn1528-8900
    keywordsCompressors
    keywordsTime series
    keywordsTravel
    keywordsWave energy
    keywordsData acquisition
    keywordsPressure transducers
    keywordsFluctuations (Physics)
    keywordsRotors
    keywordsDynamics (Mechanics)
    keywordsPressure AND Sensors
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 003
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian