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    Active Control of Combustion for Optimal Performance

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003::page 437
    Author:
    M. D. Jackson
    ,
    A. K. Agrawal
    DOI: 10.1115/1.2818492
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Combustion-zone stoichiometry and fuel-air premixing were actively controlled to optimize the combustor performance over a range of operating conditions. The objective was to maximize the combustion temperature, while maintaining NOx within a specified limit. The combustion system consisted of a premixer located coaxially near the inlet of a water-cooled shroud. The equivalence ratio was controlled by a variable-speed suction fan located downstream. The split between the premixing air and diffusion air was governed by the distance between the premixer and shroud. The combustor performance was characterized by a cost function evaluated from time-averaged measurements of NOx and oxygen concentrations in products. The cost function was minimized by the downhill simplex algorithm employing closed-loop feedback. Experiments were conducted at different fuel flow rates to demonstrate that the controller optimized the performance without prior knowledge of the combustor behavior.
    keyword(s): Combustion , Combustion chambers , Fuels , Suction , Algorithms , Combustion systems , Feedback , Oxygen , Stoichiometry , Water , Measurement , Control equipment , Flow (Dynamics) , Temperature AND Diffusion (Physics) ,
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      Active Control of Combustion for Optimal Performance

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/122117
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. D. Jackson
    contributor authorA. K. Agrawal
    date accessioned2017-05-08T23:59:33Z
    date available2017-05-08T23:59:33Z
    date copyrightJuly, 1999
    date issued1999
    identifier issn1528-8919
    identifier otherJETPEZ-26790#437_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122117
    description abstractCombustion-zone stoichiometry and fuel-air premixing were actively controlled to optimize the combustor performance over a range of operating conditions. The objective was to maximize the combustion temperature, while maintaining NOx within a specified limit. The combustion system consisted of a premixer located coaxially near the inlet of a water-cooled shroud. The equivalence ratio was controlled by a variable-speed suction fan located downstream. The split between the premixing air and diffusion air was governed by the distance between the premixer and shroud. The combustor performance was characterized by a cost function evaluated from time-averaged measurements of NOx and oxygen concentrations in products. The cost function was minimized by the downhill simplex algorithm employing closed-loop feedback. Experiments were conducted at different fuel flow rates to demonstrate that the controller optimized the performance without prior knowledge of the combustor behavior.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleActive Control of Combustion for Optimal Performance
    typeJournal Paper
    journal volume121
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2818492
    journal fristpage437
    journal lastpage443
    identifier eissn0742-4795
    keywordsCombustion
    keywordsCombustion chambers
    keywordsFuels
    keywordsSuction
    keywordsAlgorithms
    keywordsCombustion systems
    keywordsFeedback
    keywordsOxygen
    keywordsStoichiometry
    keywordsWater
    keywordsMeasurement
    keywordsControl equipment
    keywordsFlow (Dynamics)
    keywordsTemperature AND Diffusion (Physics)
    treeJournal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003
    contenttypeFulltext
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