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    Long-Term Microturbine Exposure of an Advanced Alloy for Microturbine Primary Surface Recuperators

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 003::page 32301
    Author:
    Wendy J. Matthews
    ,
    Karren L. More
    ,
    Larry R. Walker
    DOI: 10.1115/1.2966419
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Haynes alloy HR-120 (Haynes and HR-120 are trademarks of Haynes International, Inc.) forms a protective oxide scale when exposed to the harsh operating environment of a microturbine primary surface recuperator. Primary surface recuperators manufactured from HR-120 are currently in use on the Capstone C65 MicroTurbine (MicroTurbine is a registered trademark of Capstone Turbine Corporation). Long-term microturbine tests of this alloy are currently being conducted at an elevated turbine exit temperature (∼100°F higher than that in a normal operation) at Capstone Turbine Corporation. Alloy samples that have been tested under steady-state microturbine operating conditions are removed after predetermined exposure intervals for characterization by Capstone Turbine Corporation in collaboration with Oak Ridge National Laboratory. Such evaluations include the characterization of surface oxide scales and the associated alloy compositional changes following a steady-state operation ranging from 1800 h to 14,500 h. Results from the microstructural and compositional analyses of these long-term steady-state engine-tested HR-120 samples are used to illustrate the progression of alloy oxidation in the microturbine operating environment.
    keyword(s): Temperature , Alloys , Engines , Microturbines , oxidation , Steady state , Reservoirs AND Testing ,
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      Long-Term Microturbine Exposure of an Advanced Alloy for Microturbine Primary Surface Recuperators

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    contributor authorWendy J. Matthews
    contributor authorKarren L. More
    contributor authorLarry R. Walker
    date accessioned2017-05-09T00:32:41Z
    date available2017-05-09T00:32:41Z
    date copyrightMay, 2009
    date issued2009
    identifier issn1528-8919
    identifier otherJETPEZ-27066#032301_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/140469
    description abstractHaynes alloy HR-120 (Haynes and HR-120 are trademarks of Haynes International, Inc.) forms a protective oxide scale when exposed to the harsh operating environment of a microturbine primary surface recuperator. Primary surface recuperators manufactured from HR-120 are currently in use on the Capstone C65 MicroTurbine (MicroTurbine is a registered trademark of Capstone Turbine Corporation). Long-term microturbine tests of this alloy are currently being conducted at an elevated turbine exit temperature (∼100°F higher than that in a normal operation) at Capstone Turbine Corporation. Alloy samples that have been tested under steady-state microturbine operating conditions are removed after predetermined exposure intervals for characterization by Capstone Turbine Corporation in collaboration with Oak Ridge National Laboratory. Such evaluations include the characterization of surface oxide scales and the associated alloy compositional changes following a steady-state operation ranging from 1800 h to 14,500 h. Results from the microstructural and compositional analyses of these long-term steady-state engine-tested HR-120 samples are used to illustrate the progression of alloy oxidation in the microturbine operating environment.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLong-Term Microturbine Exposure of an Advanced Alloy for Microturbine Primary Surface Recuperators
    typeJournal Paper
    journal volume131
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2966419
    journal fristpage32301
    identifier eissn0742-4795
    keywordsTemperature
    keywordsAlloys
    keywordsEngines
    keywordsMicroturbines
    keywordsoxidation
    keywordsSteady state
    keywordsReservoirs AND Testing
    treeJournal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 003
    contenttypeFulltext
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