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    Validation of CESI Blade Life Management System by Case Histories and in situ NDT

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 001::page 73
    Author:
    Claudia Rinaldi
    ,
    Valerio Bicego
    ,
    Pier Paolo Colombo
    DOI: 10.1115/1.2056534
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A life management system was developed for hot components of large industrial gas turbines, in the form of a software tool for predicting component lives under typical operational transients (normal and also abnormal) and steady-state periods. The method utilizes results of previous thermo-mechanical finite element and finite volume fluid mechanics analyses. The basic idea of this method is using data from structural and aero-thermal analyses (pressures and temperatures), blade life theory, and material properties as an input to algorithms, and using operational and historical data to validate the predicted damage amounts. The software developed in this project, of general applicability to all GT models, has been implemented with reference to the geometries, materials, and service conditions of a Fiat-Westinghouse model.
    keyword(s): Coatings , Blades , Computer software , oxidation , Coating processes , Temperature , Stress , Turbines AND Creep ,
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      Validation of CESI Blade Life Management System by Case Histories and in situ NDT

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    https://yetl.yabesh.ir/yetl1/handle/yetl/133718
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorClaudia Rinaldi
    contributor authorValerio Bicego
    contributor authorPier Paolo Colombo
    date accessioned2017-05-09T00:19:55Z
    date available2017-05-09T00:19:55Z
    date copyrightJanuary, 2006
    date issued2006
    identifier issn1528-8919
    identifier otherJETPEZ-26894#73_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133718
    description abstractA life management system was developed for hot components of large industrial gas turbines, in the form of a software tool for predicting component lives under typical operational transients (normal and also abnormal) and steady-state periods. The method utilizes results of previous thermo-mechanical finite element and finite volume fluid mechanics analyses. The basic idea of this method is using data from structural and aero-thermal analyses (pressures and temperatures), blade life theory, and material properties as an input to algorithms, and using operational and historical data to validate the predicted damage amounts. The software developed in this project, of general applicability to all GT models, has been implemented with reference to the geometries, materials, and service conditions of a Fiat-Westinghouse model.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleValidation of CESI Blade Life Management System by Case Histories and in situ NDT
    typeJournal Paper
    journal volume128
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2056534
    journal fristpage73
    journal lastpage80
    identifier eissn0742-4795
    keywordsCoatings
    keywordsBlades
    keywordsComputer software
    keywordsoxidation
    keywordsCoating processes
    keywordsTemperature
    keywordsStress
    keywordsTurbines AND Creep
    treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian