YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • 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

    Blade Strain Peak Localization Method With Single Transducer During Multimode Vibration

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 145 ):;issue: 010::page 101003-1
    Author:
    Zhu, Yuda
    ,
    Wang, Yanan
    ,
    Qiao, Baijie
    ,
    Luo, Xianqiang
    ,
    Chen, Xuefeng
    DOI: 10.1115/1.4062902
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The dynamic strain/stress measurement of blades provides an effective method to anticipate fatigue life and investigate of failure causes. Unlike the blade strain peak is fixed during singlemode, which can be measured by a single transducer, the strain peak distribution changes over time and space during multimode vibration situations. The existing method reconstructs the full-field strain to find the peak point with multiple transducers. In this work, a single transducer-based full-field dynamic strain reconstruction technique is presented to find the strain peak position on rotor blades. First, the mode response is obtained by separating the measured response from a single strain gauge based on Ensemble Empirical Mode Decomposition. Second, based on the strain mode shape from the finite element model, the reconstructed strain transmissibility matrix is created between a single measured location and the full field. Third, the dynamic strain of the blade can be reconstructed at any location and time by combining the separated mode response with the RST matrix. Finally, the strain peak localization is identified according to the distribution of full-field dynamic strain during multimode vibration. The above process is verified by experimental data from rotor blades with the maximum error of reconstructed strain below 12% and three explicitly recognized strain peak positions.
    • Download: (3.692Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Blade Strain Peak Localization Method With Single Transducer During Multimode Vibration

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4294337
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorZhu, Yuda
    contributor authorWang, Yanan
    contributor authorQiao, Baijie
    contributor authorLuo, Xianqiang
    contributor authorChen, Xuefeng
    date accessioned2023-11-29T18:42:47Z
    date available2023-11-29T18:42:47Z
    date copyright8/31/2023 12:00:00 AM
    date issued8/31/2023 12:00:00 AM
    date issued2023-08-31
    identifier issn0742-4795
    identifier othergtp_145_10_101003.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4294337
    description abstractThe dynamic strain/stress measurement of blades provides an effective method to anticipate fatigue life and investigate of failure causes. Unlike the blade strain peak is fixed during singlemode, which can be measured by a single transducer, the strain peak distribution changes over time and space during multimode vibration situations. The existing method reconstructs the full-field strain to find the peak point with multiple transducers. In this work, a single transducer-based full-field dynamic strain reconstruction technique is presented to find the strain peak position on rotor blades. First, the mode response is obtained by separating the measured response from a single strain gauge based on Ensemble Empirical Mode Decomposition. Second, based on the strain mode shape from the finite element model, the reconstructed strain transmissibility matrix is created between a single measured location and the full field. Third, the dynamic strain of the blade can be reconstructed at any location and time by combining the separated mode response with the RST matrix. Finally, the strain peak localization is identified according to the distribution of full-field dynamic strain during multimode vibration. The above process is verified by experimental data from rotor blades with the maximum error of reconstructed strain below 12% and three explicitly recognized strain peak positions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBlade Strain Peak Localization Method With Single Transducer During Multimode Vibration
    typeJournal Paper
    journal volume145
    journal issue10
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4062902
    journal fristpage101003-1
    journal lastpage101003-11
    page11
    treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 145 ):;issue: 010
    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