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    A Procedure for Calculating Fuel Gas Blend Knock Rating for Large-Bore Gas Engines and Predicting Engine Operation

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 004::page 922
    Author:
    F. S. Schaub
    ,
    R. L. Hubbard
    DOI: 10.1115/1.3239837
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the procedure developed by Cooper-Bessemer for large-bore gas engines to calculate the knock rating of gas fuel blends and to predict with accuracy the required engine build to use that fuel with optimum detonation margin. Engine prototype test work has included fuel sensitivity tests mapped as a function of compression ratio, fuel air ratio, ignition advance, combustion air temperature, and engine rating. Success in predicting production engine operation for a given application involving a particular fuel blend has been gratifying. The basic reference method blend selected was normal butane in methane. Details are included in the paper to illustrate the problems in making sensitivity correlations between small-bore fuel research engines and large-bore production engines.
    keyword(s): Gaseous fuels , Engines , Gas engines , Fuels , Temperature , Combustion , Explosions , Engineering prototypes , Compression , Ignition AND Methane ,
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      A Procedure for Calculating Fuel Gas Blend Knock Rating for Large-Bore Gas Engines and Predicting Engine Operation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/99748
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorF. S. Schaub
    contributor authorR. L. Hubbard
    date accessioned2017-05-08T23:20:04Z
    date available2017-05-08T23:20:04Z
    date copyrightOctober, 1985
    date issued1985
    identifier issn1528-8919
    identifier otherJETPEZ-26626#922_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99748
    description abstractThis paper describes the procedure developed by Cooper-Bessemer for large-bore gas engines to calculate the knock rating of gas fuel blends and to predict with accuracy the required engine build to use that fuel with optimum detonation margin. Engine prototype test work has included fuel sensitivity tests mapped as a function of compression ratio, fuel air ratio, ignition advance, combustion air temperature, and engine rating. Success in predicting production engine operation for a given application involving a particular fuel blend has been gratifying. The basic reference method blend selected was normal butane in methane. Details are included in the paper to illustrate the problems in making sensitivity correlations between small-bore fuel research engines and large-bore production engines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Procedure for Calculating Fuel Gas Blend Knock Rating for Large-Bore Gas Engines and Predicting Engine Operation
    typeJournal Paper
    journal volume107
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239837
    journal fristpage922
    journal lastpage930
    identifier eissn0742-4795
    keywordsGaseous fuels
    keywordsEngines
    keywordsGas engines
    keywordsFuels
    keywordsTemperature
    keywordsCombustion
    keywordsExplosions
    keywordsEngineering prototypes
    keywordsCompression
    keywordsIgnition AND Methane
    treeJournal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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