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    Advanced High Temperature Gas-Cooled Reactor Systems

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 001::page 12902
    Author:
    Yasuyoshi Kato
    DOI: 10.1115/1.3098416
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Three systems have been proposed for advanced high-temperature gas-cooled reactors: a supercritical carbon dioxide (S-CO2) gas turbine power conversion system, a new microchannel heat exchanger (MCHE), and a once-through-then-out (OTTO) refueling scheme with burnable poison (BP) loading. A S-CO2 gas turbine cycle attains higher cycle efficiency than a He gas turbine cycle because of reduced compression work around the critical point of CO2. Considering temperature reduction at the turbine inlet by 30°C through intermediate heat exchange, the S-CO2 indirect cycle achieves an efficiency of 53.8% at a turbine inlet temperature of 820°C and a turbine inlet pressure of 20 MPa. This cycle efficiency value is higher by 4.5% than that (49.3%) of a He direct cycle at a turbine inlet temperature of 850°C and 7 MPa. A new MCHE has been proposed as an intermediate heat exchanger between the primary cooling He loop and the secondary S-CO2 gas turbine power conversion system and as recuperators of the S-CO2 gas turbine power conversion system. This MCHE has discontinuous “S-shaped” fins providing flow channels resembling sine curves. Its pressure drop is one-sixth that of a conventional MCHE with a zigzag flow channel configuration, but it has the same high heat transfer performance. The pressure drop reduction is ascribed to suppression of recirculation flows and eddies that appear around bend corners of the zigzag flow channels in the conventional MCHE. An optimal BP loading in an OTTO refueling scheme eliminates the shortcoming of its excessively high axial power peaking factor, reducing the power peaking factor from 4.44 to about 1.7, and inheriting advantages over the multipass scheme because it obviates reloading in addition to fuel handling and integrity checking systems. Because of the power peaking factor reduction, the maximum fuel temperatures are lower than the maximum permissible values of 1250°C for normal operation and 1600°C during a depressurization accident.
    keyword(s): Pressure , Flow (Dynamics) , Temperature , Channels (Hydraulic engineering) , Fuels , Gas turbines , Cycles , Pressure drop , Very high temperature reactors , Turbines , Particulate matter , Heat exchangers , Microchannels , Heat transfer , Accidents , Eddies (Fluid dynamics) , Fins AND Heat ,
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      Advanced High Temperature Gas-Cooled Reactor Systems

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    https://yetl.yabesh.ir/yetl1/handle/yetl/143306
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorYasuyoshi Kato
    date accessioned2017-05-09T00:37:55Z
    date available2017-05-09T00:37:55Z
    date copyrightJanuary, 2010
    date issued2010
    identifier issn1528-8919
    identifier otherJETPEZ-27089#012902_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143306
    description abstractThree systems have been proposed for advanced high-temperature gas-cooled reactors: a supercritical carbon dioxide (S-CO2) gas turbine power conversion system, a new microchannel heat exchanger (MCHE), and a once-through-then-out (OTTO) refueling scheme with burnable poison (BP) loading. A S-CO2 gas turbine cycle attains higher cycle efficiency than a He gas turbine cycle because of reduced compression work around the critical point of CO2. Considering temperature reduction at the turbine inlet by 30°C through intermediate heat exchange, the S-CO2 indirect cycle achieves an efficiency of 53.8% at a turbine inlet temperature of 820°C and a turbine inlet pressure of 20 MPa. This cycle efficiency value is higher by 4.5% than that (49.3%) of a He direct cycle at a turbine inlet temperature of 850°C and 7 MPa. A new MCHE has been proposed as an intermediate heat exchanger between the primary cooling He loop and the secondary S-CO2 gas turbine power conversion system and as recuperators of the S-CO2 gas turbine power conversion system. This MCHE has discontinuous “S-shaped” fins providing flow channels resembling sine curves. Its pressure drop is one-sixth that of a conventional MCHE with a zigzag flow channel configuration, but it has the same high heat transfer performance. The pressure drop reduction is ascribed to suppression of recirculation flows and eddies that appear around bend corners of the zigzag flow channels in the conventional MCHE. An optimal BP loading in an OTTO refueling scheme eliminates the shortcoming of its excessively high axial power peaking factor, reducing the power peaking factor from 4.44 to about 1.7, and inheriting advantages over the multipass scheme because it obviates reloading in addition to fuel handling and integrity checking systems. Because of the power peaking factor reduction, the maximum fuel temperatures are lower than the maximum permissible values of 1250°C for normal operation and 1600°C during a depressurization accident.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAdvanced High Temperature Gas-Cooled Reactor Systems
    typeJournal Paper
    journal volume132
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3098416
    journal fristpage12902
    identifier eissn0742-4795
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsChannels (Hydraulic engineering)
    keywordsFuels
    keywordsGas turbines
    keywordsCycles
    keywordsPressure drop
    keywordsVery high temperature reactors
    keywordsTurbines
    keywordsParticulate matter
    keywordsHeat exchangers
    keywordsMicrochannels
    keywordsHeat transfer
    keywordsAccidents
    keywordsEddies (Fluid dynamics)
    keywordsFins AND Heat
    treeJournal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 001
    contenttypeFulltext
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