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    Measurement of Flame Temperature and Emittance in Gas Turbine Combustors

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003::page 310
    Author:
    W. E. Hill
    ,
    N. R. Dibelius
    DOI: 10.1115/1.3445355
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The radiation heat load assumes an important role in gas turbine life and performance as firing temperatures and pressures are increased. This first phase of a program for assessing radiant heat loading was mainly concerned with devising measurement techniques. An experimental method for measuring the temperature of luminous flames with a two-color pyrometer and radiant intensity by means of a total radiation pyrometer is described. Emittance data from two combustion liner configurations is included for chamber pressures of from 2 to 7.5 atmospheres over the turbine inlet temperature range of 900 to 1950 deg F.
    keyword(s): Temperature , Combustion chambers , Gas turbines , Flames , Pyrometers , Radiation (Physics) , Stress , Combustion , Turbines , Firing (materials) , Radiant heat AND Heat ,
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      Measurement of Flame Temperature and Emittance in Gas Turbine Combustors

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/142266
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorW. E. Hill
    contributor authorN. R. Dibelius
    date accessioned2017-05-09T00:35:59Z
    date available2017-05-09T00:35:59Z
    date copyrightJuly, 1970
    date issued1970
    identifier issn1528-8919
    identifier otherJETPEZ-26687#310_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142266
    description abstractThe radiation heat load assumes an important role in gas turbine life and performance as firing temperatures and pressures are increased. This first phase of a program for assessing radiant heat loading was mainly concerned with devising measurement techniques. An experimental method for measuring the temperature of luminous flames with a two-color pyrometer and radiant intensity by means of a total radiation pyrometer is described. Emittance data from two combustion liner configurations is included for chamber pressures of from 2 to 7.5 atmospheres over the turbine inlet temperature range of 900 to 1950 deg F.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMeasurement of Flame Temperature and Emittance in Gas Turbine Combustors
    typeJournal Paper
    journal volume92
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445355
    journal fristpage310
    journal lastpage314
    identifier eissn0742-4795
    keywordsTemperature
    keywordsCombustion chambers
    keywordsGas turbines
    keywordsFlames
    keywordsPyrometers
    keywordsRadiation (Physics)
    keywordsStress
    keywordsCombustion
    keywordsTurbines
    keywordsFiring (materials)
    keywordsRadiant heat AND Heat
    treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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