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    Development, Testing, and Implementation of a Gas Turbine Starting Clutch With Manual Turning Feature for U.S. Navy Ships

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 003::page 785
    Author:
    Morgan L. Hendry
    ,
    Matthew G. Hoffman
    DOI: 10.1115/1.2434347
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Most gas turbine generators rely on an automatic-engaging, free-wheel clutch to connect a starting motor to accelerate the gas turbine generator from zero to some intermediate speed to enable ignition and then provide torque assistance to a higher speed until the gas turbine is self-sustaining. The U.S. Navy has used various designs of starter motors and clutches for its gas turbine fleet. In addition, there has been a requirement to periodically borescope each gas turbine, which has necessitated removal of the starting system and clutch assembly in each instance. This paper examines the U.S. Navy experience with starting clutches and provides details of the development and testing of a synchronous-self-shifting clutch with an additional, stationary, manual turning feature to provide very slow and precise gas turbine rotor rotation for borescope purposes. This paper also gives details of the installation of the first two prototype clutches on the USS Ramage, DDG 61, operating experience for approximately four years, and possible future installations of this type of clutch in U.S. Navy gas turbine generator sets.
    keyword(s): Design , Gas turbines , Testing , Turbines , Navy , Ships , Manufacturing , Gears , Torque , Engines AND Generators ,
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      Development, Testing, and Implementation of a Gas Turbine Starting Clutch With Manual Turning Feature for U.S. Navy Ships

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/135707
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorMorgan L. Hendry
    contributor authorMatthew G. Hoffman
    date accessioned2017-05-09T00:23:39Z
    date available2017-05-09T00:23:39Z
    date copyrightJuly, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26960#785_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135707
    description abstractMost gas turbine generators rely on an automatic-engaging, free-wheel clutch to connect a starting motor to accelerate the gas turbine generator from zero to some intermediate speed to enable ignition and then provide torque assistance to a higher speed until the gas turbine is self-sustaining. The U.S. Navy has used various designs of starter motors and clutches for its gas turbine fleet. In addition, there has been a requirement to periodically borescope each gas turbine, which has necessitated removal of the starting system and clutch assembly in each instance. This paper examines the U.S. Navy experience with starting clutches and provides details of the development and testing of a synchronous-self-shifting clutch with an additional, stationary, manual turning feature to provide very slow and precise gas turbine rotor rotation for borescope purposes. This paper also gives details of the installation of the first two prototype clutches on the USS Ramage, DDG 61, operating experience for approximately four years, and possible future installations of this type of clutch in U.S. Navy gas turbine generator sets.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment, Testing, and Implementation of a Gas Turbine Starting Clutch With Manual Turning Feature for U.S. Navy Ships
    typeJournal Paper
    journal volume129
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2434347
    journal fristpage785
    journal lastpage791
    identifier eissn0742-4795
    keywordsDesign
    keywordsGas turbines
    keywordsTesting
    keywordsTurbines
    keywordsNavy
    keywordsShips
    keywordsManufacturing
    keywordsGears
    keywordsTorque
    keywordsEngines AND Generators
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 003
    contenttypeFulltext
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