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    Transient Stress Analysis and Fatigue Life Estimation of Turbine Blades

    Source: Journal of Vibration and Acoustics:;2004:;volume( 126 ):;issue: 004::page 485
    Author:
    Deepak Dhar
    ,
    J. S. Rao
    ,
    A. M. Sharan
    DOI: 10.1115/1.1804996
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper is concerned with life estimation of a turbine blade taking into account the combined effects of centrifugal stresses, vibratory stresses and thermal stresses. The stresses are determined by accounting for the rotor acceleration. The blades are subjected to aerodynamic excitation force obtained from thin cambered aerofoil theory under incompressible flow. The thermo-elastic forces are obtained from the three-dimensional non-linear heat transfer equations using the finite element analysis. The fatigue life is estimated using two well known theories, from the number of cycles in various blocks during start-up and shut-down periods of the turbine operation when the stresses peak.
    keyword(s): Force , Temperature , Stress , Turbine blades , Rotors , Blades , Equations , Fatigue life , Thermal stresses , Nozzles AND Stress analysis (Engineering) ,
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      Transient Stress Analysis and Fatigue Life Estimation of Turbine Blades

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/131026
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    • Journal of Vibration and Acoustics

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    contributor authorDeepak Dhar
    contributor authorJ. S. Rao
    contributor authorA. M. Sharan
    date accessioned2017-05-09T00:14:44Z
    date available2017-05-09T00:14:44Z
    date copyrightOctober, 2004
    date issued2004
    identifier issn1048-9002
    identifier otherJVACEK-28871#485_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131026
    description abstractThis paper is concerned with life estimation of a turbine blade taking into account the combined effects of centrifugal stresses, vibratory stresses and thermal stresses. The stresses are determined by accounting for the rotor acceleration. The blades are subjected to aerodynamic excitation force obtained from thin cambered aerofoil theory under incompressible flow. The thermo-elastic forces are obtained from the three-dimensional non-linear heat transfer equations using the finite element analysis. The fatigue life is estimated using two well known theories, from the number of cycles in various blocks during start-up and shut-down periods of the turbine operation when the stresses peak.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTransient Stress Analysis and Fatigue Life Estimation of Turbine Blades
    typeJournal Paper
    journal volume126
    journal issue4
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.1804996
    journal fristpage485
    journal lastpage495
    identifier eissn1528-8927
    keywordsForce
    keywordsTemperature
    keywordsStress
    keywordsTurbine blades
    keywordsRotors
    keywordsBlades
    keywordsEquations
    keywordsFatigue life
    keywordsThermal stresses
    keywordsNozzles AND Stress analysis (Engineering)
    treeJournal of Vibration and Acoustics:;2004:;volume( 126 ):;issue: 004
    contenttypeFulltext
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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
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