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    Design and Off-Design Characteristics of the Alternative Recuperated Gas Turbine Cycle With Divided Turbine Expansion

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002::page 428
    Author:
    Sung Hoon Hwang
    ,
    Soo Hyoung Yoon
    ,
    Tong Seop Kim
    DOI: 10.1115/1.2364195
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to fully address the characteristics of the alternative recuperated cycle with divided turbine expansion, both design and off-design analyses have been performed. Two types of mechanical design are assumed: two shaft and single shaft. In particular, optimal pressure ratio division between the high- and low-pressure turbines is evaluated for the single-shaft configuration. It is predicted that the alternative recuperated cycle hardly exhibits sensible design efficiency advantage over the conventional recuperated cycle for moderate turbine inlet conditions and with usual component performances. An advantage of the alternative cycle with single-shaft design is that thermal efficiency is less sensitive to compressor pressure ratio compared to other configurations, and we can also have flexibility in the turbine division without much efficiency loss. The part load analyses have been carried out with the aid of realistic component maps and models for off-design operation. In addition to the general fuel only control, a variable speed control is assumed as the part load operating strategy of the single-shaft configuration. Obvious advantage with the alternative cycle is observed in the variable speed operation of the single-shaft design. With this strategy, the part load efficiency of the alternative cycle is far superior to the conventional cycle. Almost constant efficiency is predicted for a wide power range.
    keyword(s): Pressure , Stress , Design , Turbines , Cycles , Compressors , Gas turbines AND Temperature ,
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      Design and Off-Design Characteristics of the Alternative Recuperated Gas Turbine Cycle With Divided Turbine Expansion

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    http://yetl.yabesh.ir/yetl1/handle/yetl/135740
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    contributor authorSung Hoon Hwang
    contributor authorSoo Hyoung Yoon
    contributor authorTong Seop Kim
    date accessioned2017-05-09T00:23:44Z
    date available2017-05-09T00:23:44Z
    date copyrightApril, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26949#428_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135740
    description abstractIn order to fully address the characteristics of the alternative recuperated cycle with divided turbine expansion, both design and off-design analyses have been performed. Two types of mechanical design are assumed: two shaft and single shaft. In particular, optimal pressure ratio division between the high- and low-pressure turbines is evaluated for the single-shaft configuration. It is predicted that the alternative recuperated cycle hardly exhibits sensible design efficiency advantage over the conventional recuperated cycle for moderate turbine inlet conditions and with usual component performances. An advantage of the alternative cycle with single-shaft design is that thermal efficiency is less sensitive to compressor pressure ratio compared to other configurations, and we can also have flexibility in the turbine division without much efficiency loss. The part load analyses have been carried out with the aid of realistic component maps and models for off-design operation. In addition to the general fuel only control, a variable speed control is assumed as the part load operating strategy of the single-shaft configuration. Obvious advantage with the alternative cycle is observed in the variable speed operation of the single-shaft design. With this strategy, the part load efficiency of the alternative cycle is far superior to the conventional cycle. Almost constant efficiency is predicted for a wide power range.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign and Off-Design Characteristics of the Alternative Recuperated Gas Turbine Cycle With Divided Turbine Expansion
    typeJournal Paper
    journal volume129
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2364195
    journal fristpage428
    journal lastpage435
    identifier eissn0742-4795
    keywordsPressure
    keywordsStress
    keywordsDesign
    keywordsTurbines
    keywordsCycles
    keywordsCompressors
    keywordsGas turbines AND Temperature
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002
    contenttypeFulltext
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