Gas turbine engine combustor technology for the reduction of pollutant emissions is summarized. Variations of conventional combustion systems and advanced combustor concepts are discussed. Projected results from far term technology efforts aimed at applying the premixed prevaporized and catalytic combustion techniques to aircraft combustion systems indicate a potential for significant reductions in pollutant emission levels.


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    Title :

    Advanced technology for controlling pollutant emissions from supersonic cruise aircraft


    Contributors:
    Duerr, R. A. (author) / Diehl, L. A. (author)


    Publication date :

    1980-03-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English