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    Shop Test Result of the V64.3 Gas Turbine

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 004::page 676
    Author:
    M. Jansen
    ,
    T. Schulenberg
    ,
    D. Waldinger
    DOI: 10.1115/1.2906641
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The V64.3 60-MW combustion turbine is the first of a new generation of high-temperature gas turbines, designed for 50 and 60 Hz simple cycle, combined cycle, and cogeneration applications. The prototype engine was tested in 1990 in the Berlin factories under the full range of operation conditions. It was equipped with various measurement systems to monitor pressures, gas and metal temperatures, clearances, strains, vibrations, and exhaust emissions. The paper describes the engine design, the test facility and instrumentation, and the engine performance. Results are given for turbine blade temperatures, compressor and turbine vibrations, exhaust gas temperature, and NOx emissions for combustion of natural gas and fuel oil.
    keyword(s): Gas turbines , Temperature , Combustion , Engines , Turbines , Vibration , Cycles , Exhaust systems , Emissions , High temperature , Measurement systems , Test facilities , Engine design , Combined heat and power , Instrumentation , Natural gas , Compressors , Turbine blades , Engineering prototypes , Metals AND Fuel oils ,
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      Shop Test Result of the V64.3 Gas Turbine

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/110166
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. Jansen
    contributor authorT. Schulenberg
    contributor authorD. Waldinger
    date accessioned2017-05-08T23:38:16Z
    date available2017-05-08T23:38:16Z
    date copyrightOctober, 1992
    date issued1992
    identifier issn1528-8919
    identifier otherJETPEZ-26709#676_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110166
    description abstractThe V64.3 60-MW combustion turbine is the first of a new generation of high-temperature gas turbines, designed for 50 and 60 Hz simple cycle, combined cycle, and cogeneration applications. The prototype engine was tested in 1990 in the Berlin factories under the full range of operation conditions. It was equipped with various measurement systems to monitor pressures, gas and metal temperatures, clearances, strains, vibrations, and exhaust emissions. The paper describes the engine design, the test facility and instrumentation, and the engine performance. Results are given for turbine blade temperatures, compressor and turbine vibrations, exhaust gas temperature, and NOx emissions for combustion of natural gas and fuel oil.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleShop Test Result of the V64.3 Gas Turbine
    typeJournal Paper
    journal volume114
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906641
    journal fristpage676
    journal lastpage681
    identifier eissn0742-4795
    keywordsGas turbines
    keywordsTemperature
    keywordsCombustion
    keywordsEngines
    keywordsTurbines
    keywordsVibration
    keywordsCycles
    keywordsExhaust systems
    keywordsEmissions
    keywordsHigh temperature
    keywordsMeasurement systems
    keywordsTest facilities
    keywordsEngine design
    keywordsCombined heat and power
    keywordsInstrumentation
    keywordsNatural gas
    keywordsCompressors
    keywordsTurbine blades
    keywordsEngineering prototypes
    keywordsMetals AND Fuel oils
    treeJournal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 004
    contenttypeFulltext
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