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    Life Assessment of Turbine Components Through Experimental and Numerical Investigations

    Source: Journal of Pressure Vessel Technology:;2013:;volume( 135 ):;issue: 002::page 24502
    Author:
    Hu, Dianyin
    ,
    Wang, Rongqiao
    ,
    Hou, Guicang
    DOI: 10.1115/1.4007962
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new lifetime criterion for withdrawal of turbine components from service is developed in this paper based on finite element (FE) analysis and experimental results. Finite element analysis is used to determine stresses in the turbine component during the imposed cyclic loads and analytically predict a fatigue life. Based on the finite element analysis, the critical section is then subjected to a creepfatigue test, using three groups of full scale turbine components, attached to an actual turbine disc conducted at 750 آ°C. The experimental data and life prediction results were in good agreement. The creepfatigue life of this type of turbine component at a 99.87% survival rate is 30 h.
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      Life Assessment of Turbine Components Through Experimental and Numerical Investigations

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    http://yetl.yabesh.ir/yetl1/handle/yetl/153013
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    contributor authorHu, Dianyin
    contributor authorWang, Rongqiao
    contributor authorHou, Guicang
    date accessioned2017-05-09T01:02:13Z
    date available2017-05-09T01:02:13Z
    date issued2013
    identifier issn0094-9930
    identifier otherpvt_135_2_024502.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153013
    description abstractA new lifetime criterion for withdrawal of turbine components from service is developed in this paper based on finite element (FE) analysis and experimental results. Finite element analysis is used to determine stresses in the turbine component during the imposed cyclic loads and analytically predict a fatigue life. Based on the finite element analysis, the critical section is then subjected to a creepfatigue test, using three groups of full scale turbine components, attached to an actual turbine disc conducted at 750 آ°C. The experimental data and life prediction results were in good agreement. The creepfatigue life of this type of turbine component at a 99.87% survival rate is 30 h.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLife Assessment of Turbine Components Through Experimental and Numerical Investigations
    typeJournal Paper
    journal volume135
    journal issue2
    journal titleJournal of Pressure Vessel Technology
    identifier doi10.1115/1.4007962
    journal fristpage24502
    journal lastpage24502
    identifier eissn1528-8978
    treeJournal of Pressure Vessel Technology:;2013:;volume( 135 ):;issue: 002
    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
    yabeshDSpacePersian