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    Aircraft Gas Turbine Emissions Challenge

    Source: Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003::page 474
    Author:
    B. L. Koff
    DOI: 10.1115/1.2906845
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The new generation of jet powered aircraft faces a significant challenge to reduce pollutant emissions while increasing fuel efficiency. Carbon monoxide (CO) and unburned hydrocarbon (HC) emissions are already very low and continued control of these pollutants is expected as engine temperatures and pressure ratios are increased. In contrast, significant system design improvements are needed to reduce oxides of nitrogen (NOx ) emissions because of their harmful effect on the earth’s ozone layer. This paper discusses the prospects and technical approaches for significant NOx reductions in current and future subsonic and supersonic aircraft.
    keyword(s): Gas turbines , Aircraft , Emissions , Pollution , Fuel efficiency , Nitrogen , Pressure , Temperature , Engines , Carbon AND Design ,
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      Aircraft Gas Turbine Emissions Challenge

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    http://yetl.yabesh.ir/yetl1/handle/yetl/113531
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    contributor authorB. L. Koff
    date accessioned2017-05-08T23:44:05Z
    date available2017-05-08T23:44:05Z
    date copyrightJuly, 1994
    date issued1994
    identifier issn1528-8919
    identifier otherJETPEZ-26729#474_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113531
    description abstractThe new generation of jet powered aircraft faces a significant challenge to reduce pollutant emissions while increasing fuel efficiency. Carbon monoxide (CO) and unburned hydrocarbon (HC) emissions are already very low and continued control of these pollutants is expected as engine temperatures and pressure ratios are increased. In contrast, significant system design improvements are needed to reduce oxides of nitrogen (NOx ) emissions because of their harmful effect on the earth’s ozone layer. This paper discusses the prospects and technical approaches for significant NOx reductions in current and future subsonic and supersonic aircraft.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAircraft Gas Turbine Emissions Challenge
    typeJournal Paper
    journal volume116
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906845
    journal fristpage474
    journal lastpage477
    identifier eissn0742-4795
    keywordsGas turbines
    keywordsAircraft
    keywordsEmissions
    keywordsPollution
    keywordsFuel efficiency
    keywordsNitrogen
    keywordsPressure
    keywordsTemperature
    keywordsEngines
    keywordsCarbon AND Design
    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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