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.
The Impact of Emission Standards on the Design of Aircraft Gas Turbine Engine Combustors
Sae Technical Papers
Aerospace Engineering and Manufacturing Meeting ; 1976
01.02.1976
Aufsatz (Konferenz)
Englisch
Aircraft turbine engine combustors - development status/challenges
Tema Archiv | 1992
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