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    Evaluation of Thermal Aging Embrittlement in Directionally Solidified Ni-Base Superalloy by Small Punch Test

    Source: Journal of Engineering Materials and Technology:;2005:;volume( 127 ):;issue: 004::page 476
    Author:
    Shin-ichi Komazaki
    ,
    Tetsuo Shoji
    ,
    Kazumune Takamura
    DOI: 10.1115/1.2019983
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to develop a procedure for evaluating the degradation of impact toughness in directionally solidified Ni-base superalloy CM247LC, which is commonly used for advanced gas turbine blades, the change in small punch (SP) fracture energy due to thermal aging has been investigated. The SP testing technique has been applied to materials aged under various aging conditions, and correlation with the results of Charpy V-notch impact tests has been examined. The experimental results reveal that SP fracture energy at room temperature decreases with aging at 800 °C and is uniquely correlated with high-temperature Charpy impact toughness. The current experiment has shown that the SP testing technique is useful in evaluating the degree of thermal aging embrittlement, one of the parameters required for remaining-life prediction of aged components.
    keyword(s): Temperature , Superalloys , Fracture (Process) , Embrittlement , Toughness , High temperature , Testing , Blades , Impact testing , Stress , Casting AND Gas turbines ,
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      Evaluation of Thermal Aging Embrittlement in Directionally Solidified Ni-Base Superalloy by Small Punch Test

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/131848
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    • Journal of Engineering Materials and Technology

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    contributor authorShin-ichi Komazaki
    contributor authorTetsuo Shoji
    contributor authorKazumune Takamura
    date accessioned2017-05-09T00:16:15Z
    date available2017-05-09T00:16:15Z
    date copyrightOctober, 2005
    date issued2005
    identifier issn0094-4289
    identifier otherJEMTA8-27074#476_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131848
    description abstractIn order to develop a procedure for evaluating the degradation of impact toughness in directionally solidified Ni-base superalloy CM247LC, which is commonly used for advanced gas turbine blades, the change in small punch (SP) fracture energy due to thermal aging has been investigated. The SP testing technique has been applied to materials aged under various aging conditions, and correlation with the results of Charpy V-notch impact tests has been examined. The experimental results reveal that SP fracture energy at room temperature decreases with aging at 800 °C and is uniquely correlated with high-temperature Charpy impact toughness. The current experiment has shown that the SP testing technique is useful in evaluating the degree of thermal aging embrittlement, one of the parameters required for remaining-life prediction of aged components.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEvaluation of Thermal Aging Embrittlement in Directionally Solidified Ni-Base Superalloy by Small Punch Test
    typeJournal Paper
    journal volume127
    journal issue4
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.2019983
    journal fristpage476
    journal lastpage482
    identifier eissn1528-8889
    keywordsTemperature
    keywordsSuperalloys
    keywordsFracture (Process)
    keywordsEmbrittlement
    keywordsToughness
    keywordsHigh temperature
    keywordsTesting
    keywordsBlades
    keywordsImpact testing
    keywordsStress
    keywordsCasting AND Gas turbines
    treeJournal of Engineering Materials and Technology:;2005:;volume( 127 ):;issue: 004
    contenttypeFulltext
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