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    Stability Analysis and Testing of a Train of Centrifugal Compressors for High Pressure Gas Injection

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003::page 509
    Author:
    E. A. Memmott
    DOI: 10.1115/1.2818502
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the rotor dynamic stability analysis and the PTC-10 Class 1 test of a three body centrifugal compressor train for high pressure natural gas injection service. This train had a full load full pressure string test on hydrocarbon gasses to a final discharge pressure of 500 BAR (7250 PSIA). Each compressor is of the back to back configuration, and is equipped with tilting pad seals, damper bearings, and a honeycomb labyrinth at the division wall with shunt holes. The driver is a gas turbine.
    keyword(s): Stability , Compressors , High pressure (Physics) , Testing , Trains , Pressure , Dynamic stability , Bearings , Dampers , Gas turbines , Natural gas , Rotors , String AND Stress ,
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      Stability Analysis and Testing of a Train of Centrifugal Compressors for High Pressure Gas Injection

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/122128
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorE. A. Memmott
    date accessioned2017-05-08T23:59:35Z
    date available2017-05-08T23:59:35Z
    date copyrightJuly, 1999
    date issued1999
    identifier issn1528-8919
    identifier otherJETPEZ-26790#509_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122128
    description abstractThis paper describes the rotor dynamic stability analysis and the PTC-10 Class 1 test of a three body centrifugal compressor train for high pressure natural gas injection service. This train had a full load full pressure string test on hydrocarbon gasses to a final discharge pressure of 500 BAR (7250 PSIA). Each compressor is of the back to back configuration, and is equipped with tilting pad seals, damper bearings, and a honeycomb labyrinth at the division wall with shunt holes. The driver is a gas turbine.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStability Analysis and Testing of a Train of Centrifugal Compressors for High Pressure Gas Injection
    typeJournal Paper
    journal volume121
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2818502
    journal fristpage509
    journal lastpage514
    identifier eissn0742-4795
    keywordsStability
    keywordsCompressors
    keywordsHigh pressure (Physics)
    keywordsTesting
    keywordsTrains
    keywordsPressure
    keywordsDynamic stability
    keywordsBearings
    keywordsDampers
    keywordsGas turbines
    keywordsNatural gas
    keywordsRotors
    keywordsString AND Stress
    treeJournal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003
    contenttypeFulltext
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