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    Low Emissions Combustion for the Regenerative Gas Turbine: Part 2—Experimental Techniques, Results, and Assessment

    Source: Journal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 001::page 49
    Author:
    N. A. Azelborn
    ,
    W. R. Wade
    ,
    J. R. Secord
    ,
    A. F. McLean
    DOI: 10.1115/1.3445747
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This second part, of a two part paper, describes an experimental program to demonstrate the low emissions turbine combustor concept developed in Part 1. The paper discusses the combustor test rigs and instrumentation used as well as the experimental combustor hardware. A summary of the lean homogeneous combustion concept is presented along with a brief discussion of the requirement for variable combustor geometry. Test data are presented comparing the emissions from the experimental combustor with those from a conventional can-type combustor. These results show that, over a wide range of engine conditions, the steady-state emissions of NOx , CO, and UHC are below the numerical levels specified in the Federal standards applicable to 1976 and subsequent model year light duty vehicles. The results are related to theoretical calculations and an assessment of progress and remaining problems is made.
    keyword(s): Gas turbines , Combustion , Emissions , Combustion chambers , Engines , Hardware , Instrumentation , Turbines , Geometry , Steady state AND Light trucks ,
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      Low Emissions Combustion for the Regenerative Gas Turbine: Part 2—Experimental Techniques, Results, and Assessment

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/164778
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorN. A. Azelborn
    contributor authorW. R. Wade
    contributor authorJ. R. Secord
    contributor authorA. F. McLean
    date accessioned2017-05-09T01:38:09Z
    date available2017-05-09T01:38:09Z
    date copyrightJanuary, 1974
    date issued1974
    identifier issn1528-8919
    identifier otherJETPEZ-26707#49_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/164778
    description abstractThis second part, of a two part paper, describes an experimental program to demonstrate the low emissions turbine combustor concept developed in Part 1. The paper discusses the combustor test rigs and instrumentation used as well as the experimental combustor hardware. A summary of the lean homogeneous combustion concept is presented along with a brief discussion of the requirement for variable combustor geometry. Test data are presented comparing the emissions from the experimental combustor with those from a conventional can-type combustor. These results show that, over a wide range of engine conditions, the steady-state emissions of NOx , CO, and UHC are below the numerical levels specified in the Federal standards applicable to 1976 and subsequent model year light duty vehicles. The results are related to theoretical calculations and an assessment of progress and remaining problems is made.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLow Emissions Combustion for the Regenerative Gas Turbine: Part 2—Experimental Techniques, Results, and Assessment
    typeJournal Paper
    journal volume96
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445747
    journal fristpage49
    journal lastpage55
    identifier eissn0742-4795
    keywordsGas turbines
    keywordsCombustion
    keywordsEmissions
    keywordsCombustion chambers
    keywordsEngines
    keywordsHardware
    keywordsInstrumentation
    keywordsTurbines
    keywordsGeometry
    keywordsSteady state AND Light trucks
    treeJournal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 001
    contenttypeFulltext
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