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    Primary Surface Recuperator Alloy Oxidation: A Comparison of Accelerated Engine Testing to Field Operation

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 004::page 42302
    Author:
    Wendy J. Matthews
    ,
    Karren L. More
    ,
    Larry R. Walker
    DOI: 10.1115/1.4002174
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The Capstone C65 Microturbine primary surface recuperator (PSR) core has been manufactured from Haynes alloy HR-120 since 2005 (Microturbine is a registered trademark of Capstone Turbine Corporation; Haynes and HR-120 are trademarks of Haynes International, Inc.). When exposed to the harsh operating environment of the microturbine PSR, HR-120 forms a protective oxide scale that is resistant to the effects of the water vapor present in the exhaust gas. Long-term accelerated microturbine testing with samples in a modified PSR with a removable aft dome is ongoing at an elevated turbine exit temperature (TET) ∼100°F higher than normal operation. The elevated TET test engine is operated at steady-state conditions, and the engine is shut down at predetermined intervals for sample removal. Material characterization of the elevated TET samples has been carried out by Capstone Turbine Corporation in collaboration with Oak Ridge National Laboratory. The surface oxide scale formation and associated alloy compositional changes have been evaluated for elevated TET samples with operating lives ranging from ∼1800 h to ∼26,500 h. In addition, field-operated HR-120 recuperators have been sectioned and samples have been evaluated for operating lives ranging from ∼5500 h to ∼18,000 h. Results from the microstructural and compositional analyses of both the long-term steady-state elevated TET HR-120 samples and the field-operated HR-120 recuperator samples will be presented and compared.
    keyword(s): Temperature , Alloys , Engines , Testing , oxidation , Steady state , Microturbines AND Turbines ,
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      Primary Surface Recuperator Alloy Oxidation: A Comparison of Accelerated Engine Testing to Field Operation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/146053
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorWendy J. Matthews
    contributor authorKarren L. More
    contributor authorLarry R. Walker
    date accessioned2017-05-09T00:43:44Z
    date available2017-05-09T00:43:44Z
    date copyrightApril, 2011
    date issued2011
    identifier issn1528-8919
    identifier otherJETPEZ-27161#042302_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/146053
    description abstractThe Capstone C65 Microturbine primary surface recuperator (PSR) core has been manufactured from Haynes alloy HR-120 since 2005 (Microturbine is a registered trademark of Capstone Turbine Corporation; Haynes and HR-120 are trademarks of Haynes International, Inc.). When exposed to the harsh operating environment of the microturbine PSR, HR-120 forms a protective oxide scale that is resistant to the effects of the water vapor present in the exhaust gas. Long-term accelerated microturbine testing with samples in a modified PSR with a removable aft dome is ongoing at an elevated turbine exit temperature (TET) ∼100°F higher than normal operation. The elevated TET test engine is operated at steady-state conditions, and the engine is shut down at predetermined intervals for sample removal. Material characterization of the elevated TET samples has been carried out by Capstone Turbine Corporation in collaboration with Oak Ridge National Laboratory. The surface oxide scale formation and associated alloy compositional changes have been evaluated for elevated TET samples with operating lives ranging from ∼1800 h to ∼26,500 h. In addition, field-operated HR-120 recuperators have been sectioned and samples have been evaluated for operating lives ranging from ∼5500 h to ∼18,000 h. Results from the microstructural and compositional analyses of both the long-term steady-state elevated TET HR-120 samples and the field-operated HR-120 recuperator samples will be presented and compared.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePrimary Surface Recuperator Alloy Oxidation: A Comparison of Accelerated Engine Testing to Field Operation
    typeJournal Paper
    journal volume133
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4002174
    journal fristpage42302
    identifier eissn0742-4795
    keywordsTemperature
    keywordsAlloys
    keywordsEngines
    keywordsTesting
    keywordsoxidation
    keywordsSteady state
    keywordsMicroturbines AND Turbines
    treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 004
    contenttypeFulltext
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