The advent of environmental standards for controlling aircraft gas turbine engine emissions has led to a reevaluation of combustor design techniques. Effective emission control techniques have been identified and a wide spectrum of potential applications for these techniques to existing and advanced engines are being considered. Results from advanced combustor concept evaluations and from fundamental experiments are presented and discussed and comparisons are made with existing EPA emission standards and recommended levels for high altitude cruise. The impact that the advanced low emission concepts may impose on future aircraft engine combustor designs and related engine components is discussed.


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    Title :

    The impact of emission standards on the design of aircraft gas turbine engine combustors


    Contributors:

    Conference:

    Aerospace Engineering and Manufacturing Meeting on Cyclic structural analyses of air-cooled gas turbine blades and vanes ; 1976 ; San Diego, CA


    Publication date :

    1976-11-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English