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    Life Assessment of an HP-IP Rotor Under Creep Service Conditions

    Source: Journal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 002::page 237
    Author:
    V. P. Swaminathan
    ,
    N. S. Cheruvu
    ,
    A. Saxena
    DOI: 10.1115/1.2906169
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A CrMoV high and intermediate-pressure (HP-IP) rotor exhibited in-service cracking in the blade groove walls. Cracks initiated from a notch and propagated under creep conditions to a depth of 0.255 in. (6.5 mm). Since the unit was base loaded, the contribution of cyclic loading (startups and shutdowns) was not significant. The total life of the groove walls is predicted by applying a life prediction approach that accounts for both crack initiation and propagation. Crack initiation life is based on short-term creep tests extrapolated to long times using a time-temperature parameter. Crack propagation time is estimated using a newly developed time-dependent fracture mechanics concept. A parameter Ct is used to express the crack growth rate under creep loading conditions. Pertinent material properties such as creep deformation and creep crack growth rate were obtained by testing the material from the subject rotor. The results obtained by this analysis show that about 50 percent of the estimated life was spent in crack propagation. Predicted service life time compares very favorably with the actual operating life of the rotor.
    keyword(s): Creep , Rotors , Fracture (Materials) , Service life (Equipment) , Crack propagation , Pressure , Fracture mechanics , Temperature , Materials properties , Fracture (Process) , Testing AND Blades ,
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      Life Assessment of an HP-IP Rotor Under Creep Service Conditions

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    http://yetl.yabesh.ir/yetl1/handle/yetl/106930
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorV. P. Swaminathan
    contributor authorN. S. Cheruvu
    contributor authorA. Saxena
    date accessioned2017-05-08T23:32:37Z
    date available2017-05-08T23:32:37Z
    date copyrightApril, 1990
    date issued1990
    identifier issn1528-8919
    identifier otherJETPEZ-26676#237_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106930
    description abstractA CrMoV high and intermediate-pressure (HP-IP) rotor exhibited in-service cracking in the blade groove walls. Cracks initiated from a notch and propagated under creep conditions to a depth of 0.255 in. (6.5 mm). Since the unit was base loaded, the contribution of cyclic loading (startups and shutdowns) was not significant. The total life of the groove walls is predicted by applying a life prediction approach that accounts for both crack initiation and propagation. Crack initiation life is based on short-term creep tests extrapolated to long times using a time-temperature parameter. Crack propagation time is estimated using a newly developed time-dependent fracture mechanics concept. A parameter Ct is used to express the crack growth rate under creep loading conditions. Pertinent material properties such as creep deformation and creep crack growth rate were obtained by testing the material from the subject rotor. The results obtained by this analysis show that about 50 percent of the estimated life was spent in crack propagation. Predicted service life time compares very favorably with the actual operating life of the rotor.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLife Assessment of an HP-IP Rotor Under Creep Service Conditions
    typeJournal Paper
    journal volume112
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906169
    journal fristpage237
    journal lastpage242
    identifier eissn0742-4795
    keywordsCreep
    keywordsRotors
    keywordsFracture (Materials)
    keywordsService life (Equipment)
    keywordsCrack propagation
    keywordsPressure
    keywordsFracture mechanics
    keywordsTemperature
    keywordsMaterials properties
    keywordsFracture (Process)
    keywordsTesting AND Blades
    treeJournal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 002
    contenttypeFulltext
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