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    Control Requirements for the RB 211 Low-Emission Combustion System

    Source: Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003::page 527
    Author:
    N. C. Corbett
    ,
    N. P. Lines
    DOI: 10.1115/1.2906851
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The RB 211 DLE series staged, premix, lean burn combustor demands total integration of control system and combustion hardware. The controls design process is described from the conception of the Engine Management System (EMS), which provides protection and control in separate environments, through to implementation of engine development testing. The process of devising an acceptable fueling strategy to each combustion stage is discussed. This identified the requirements for the computation of complex routines in order to control combustion zone temperatures. The sensitivity of the control design to external conditions of humidity, ambient temperature, and fuel composition is explored. Extensive simulation was used to determine necessary instrumentation accuracies. The paper concludes with a review of the development testing and the final control system configuration.
    keyword(s): Temperature , Combustion , Control systems , Fuels , Engines , Simulation , Hardware , Combustion chambers , Combustion systems , Design , Instrumentation , Testing , Computation AND Emissions ,
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      Control Requirements for the RB 211 Low-Emission Combustion System

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    http://yetl.yabesh.ir/yetl1/handle/yetl/113538
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorN. C. Corbett
    contributor authorN. P. Lines
    date accessioned2017-05-08T23:44:06Z
    date available2017-05-08T23:44:06Z
    date copyrightJuly, 1994
    date issued1994
    identifier issn1528-8919
    identifier otherJETPEZ-26729#527_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113538
    description abstractThe RB 211 DLE series staged, premix, lean burn combustor demands total integration of control system and combustion hardware. The controls design process is described from the conception of the Engine Management System (EMS), which provides protection and control in separate environments, through to implementation of engine development testing. The process of devising an acceptable fueling strategy to each combustion stage is discussed. This identified the requirements for the computation of complex routines in order to control combustion zone temperatures. The sensitivity of the control design to external conditions of humidity, ambient temperature, and fuel composition is explored. Extensive simulation was used to determine necessary instrumentation accuracies. The paper concludes with a review of the development testing and the final control system configuration.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleControl Requirements for the RB 211 Low-Emission Combustion System
    typeJournal Paper
    journal volume116
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906851
    journal fristpage527
    journal lastpage533
    identifier eissn0742-4795
    keywordsTemperature
    keywordsCombustion
    keywordsControl systems
    keywordsFuels
    keywordsEngines
    keywordsSimulation
    keywordsHardware
    keywordsCombustion chambers
    keywordsCombustion systems
    keywordsDesign
    keywordsInstrumentation
    keywordsTesting
    keywordsComputation AND Emissions
    treeJournal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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