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    Design Considerations for Supercritical Carbon Dioxide Brayton Cycles With Recompression

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 010::page 101701
    Author:
    Dyreby, John
    ,
    Klein, Sanford
    ,
    Nellis, Gregory
    ,
    Reindl, Douglas
    DOI: 10.1115/1.4027936
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Supercritical carbon dioxide (SCO2) Brayton cycles have the potential to offer improved thermaltoelectric conversion efficiency for utility scale electricity production. These cycles have generated considerable interest in recent years because of this potential and are being considered for a range of applications, including nuclear and concentrating solar power (CSP). Two promising SCO2 power cycle variations are the simple Brayton cycle with recuperation and the recompression cycle. The models described in this paper are appropriate for the analysis and optimization of both cycle configurations under a range of design conditions. The recuperators in the cycle are modeled assuming a constant heat exchanger conductance value, which allows for computationally efficient optimization of the cycle's design parameters while accounting for the rapidly varying fluid properties of carbon dioxide near its critical point. Representing the recuperators using conductance, rather than effectiveness, allows for a more appropriate comparison among designpoint conditions because a larger conductance typically corresponds more directly to a physically larger and higher capital cost heat exchanger. The model is used to explore the relationship between recuperator size and heat rejection temperature of the cycle, specifically in regard to maximizing thermal efficiency. The results presented in this paper are normalized by net power output and may be applied to cycles of any size. Under the design conditions considered for this analysis, results indicate that increasing the design highside (compressor outlet) pressure does not always correspond to higher cycle thermal efficiency. Rather, there is an optimal compressor outlet pressure that is dependent on the recuperator size and operating temperatures of the cycle and is typically in the range of 30–35 MPa. Model results also indicate that the efficiency degradation associated with warmer heat rejection temperatures (e.g., in drycooled applications) are reduced by increasing the compressor inlet pressure. Because the optimal design of a cycle depends upon a number of applicationspecific variables, the model presented in this paper is available online and is envisioned as a building block for more complex and specific simulations.
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      Design Considerations for Supercritical Carbon Dioxide Brayton Cycles With Recompression

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    http://yetl.yabesh.ir/yetl1/handle/yetl/154822
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    contributor authorDyreby, John
    contributor authorKlein, Sanford
    contributor authorNellis, Gregory
    contributor authorReindl, Douglas
    date accessioned2017-05-09T01:08:00Z
    date available2017-05-09T01:08:00Z
    date issued2014
    identifier issn1528-8919
    identifier othergtp_136_10_101701.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154822
    description abstractSupercritical carbon dioxide (SCO2) Brayton cycles have the potential to offer improved thermaltoelectric conversion efficiency for utility scale electricity production. These cycles have generated considerable interest in recent years because of this potential and are being considered for a range of applications, including nuclear and concentrating solar power (CSP). Two promising SCO2 power cycle variations are the simple Brayton cycle with recuperation and the recompression cycle. The models described in this paper are appropriate for the analysis and optimization of both cycle configurations under a range of design conditions. The recuperators in the cycle are modeled assuming a constant heat exchanger conductance value, which allows for computationally efficient optimization of the cycle's design parameters while accounting for the rapidly varying fluid properties of carbon dioxide near its critical point. Representing the recuperators using conductance, rather than effectiveness, allows for a more appropriate comparison among designpoint conditions because a larger conductance typically corresponds more directly to a physically larger and higher capital cost heat exchanger. The model is used to explore the relationship between recuperator size and heat rejection temperature of the cycle, specifically in regard to maximizing thermal efficiency. The results presented in this paper are normalized by net power output and may be applied to cycles of any size. Under the design conditions considered for this analysis, results indicate that increasing the design highside (compressor outlet) pressure does not always correspond to higher cycle thermal efficiency. Rather, there is an optimal compressor outlet pressure that is dependent on the recuperator size and operating temperatures of the cycle and is typically in the range of 30–35 MPa. Model results also indicate that the efficiency degradation associated with warmer heat rejection temperatures (e.g., in drycooled applications) are reduced by increasing the compressor inlet pressure. Because the optimal design of a cycle depends upon a number of applicationspecific variables, the model presented in this paper is available online and is envisioned as a building block for more complex and specific simulations.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign Considerations for Supercritical Carbon Dioxide Brayton Cycles With Recompression
    typeJournal Paper
    journal volume136
    journal issue10
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4027936
    journal fristpage101701
    journal lastpage101701
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 010
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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