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    Simulation of an Advanced Twin-Spool Industrial Gas Turbine

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002::page 180
    Author:
    Ping Zhu
    ,
    H. I. H. Saravanamuttoo
    DOI: 10.1115/1.2906568
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A full-range mathematical model of the LM-1600 gas turbine has been developed, for future use in EHM studies. No data were available from the manufacturer other than sales brochures giving some design and off-design performance. The model was developed using generalized component characteristics and shows excellent agreement with field data from a pipeline operator. A new method has been developed for doing the matching calculations, starting from the turbine (hot) end rather than from the compressor operating point. This method permits solution on a PC, and can be used for studying the full range of operating conditions and the development of fault matrices.
    keyword(s): Simulation , Industrial gases , Turbines , Design , Gas turbines , Pipelines , Sales AND Compressors ,
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      Simulation of an Advanced Twin-Spool Industrial Gas Turbine

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/110221
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorPing Zhu
    contributor authorH. I. H. Saravanamuttoo
    date accessioned2017-05-08T23:38:25Z
    date available2017-05-08T23:38:25Z
    date copyrightApril, 1992
    date issued1992
    identifier issn1528-8919
    identifier otherJETPEZ-26699#180_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110221
    description abstractA full-range mathematical model of the LM-1600 gas turbine has been developed, for future use in EHM studies. No data were available from the manufacturer other than sales brochures giving some design and off-design performance. The model was developed using generalized component characteristics and shows excellent agreement with field data from a pipeline operator. A new method has been developed for doing the matching calculations, starting from the turbine (hot) end rather than from the compressor operating point. This method permits solution on a PC, and can be used for studying the full range of operating conditions and the development of fault matrices.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimulation of an Advanced Twin-Spool Industrial Gas Turbine
    typeJournal Paper
    journal volume114
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906568
    journal fristpage180
    journal lastpage185
    identifier eissn0742-4795
    keywordsSimulation
    keywordsIndustrial gases
    keywordsTurbines
    keywordsDesign
    keywordsGas turbines
    keywordsPipelines
    keywordsSales AND Compressors
    treeJournal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002
    contenttypeFulltext
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