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    High-Temperature Fatigue/Creep/Environment Interactions in Compressor Alloys

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001::page 246
    Author:
    W. J. Evans
    ,
    J. P. Jones
    ,
    M. R. Bache
    DOI: 10.1115/1.1498272
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The high-temperature fatigue response of titanium and nickel alloys destined for high-performance gas turbine applications is considered with particular emphasis given to the role of creep and environmental damage during crack growth. In an attempt to partition the respective contributions from these two rate controlling factors, data are presented for a range of temperature, stress ratio, and pressure conditions. The implications for the extended use of such alloys in future gas turbine designs are discussed.
    keyword(s): Creep , Fatigue , Temperature , Alloys , Stress , Fracture (Materials) , High temperature , Nickel alloys AND Compressors ,
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      High-Temperature Fatigue/Creep/Environment Interactions in Compressor Alloys

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/128437
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorW. J. Evans
    contributor authorJ. P. Jones
    contributor authorM. R. Bache
    date accessioned2017-05-09T00:10:18Z
    date available2017-05-09T00:10:18Z
    date copyrightJanuary, 2003
    date issued2003
    identifier issn1528-8919
    identifier otherJETPEZ-26819#246_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128437
    description abstractThe high-temperature fatigue response of titanium and nickel alloys destined for high-performance gas turbine applications is considered with particular emphasis given to the role of creep and environmental damage during crack growth. In an attempt to partition the respective contributions from these two rate controlling factors, data are presented for a range of temperature, stress ratio, and pressure conditions. The implications for the extended use of such alloys in future gas turbine designs are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHigh-Temperature Fatigue/Creep/Environment Interactions in Compressor Alloys
    typeJournal Paper
    journal volume125
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1498272
    journal fristpage246
    journal lastpage251
    identifier eissn0742-4795
    keywordsCreep
    keywordsFatigue
    keywordsTemperature
    keywordsAlloys
    keywordsStress
    keywordsFracture (Materials)
    keywordsHigh temperature
    keywordsNickel alloys AND Compressors
    treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001
    contenttypeFulltext
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