The Impact of Emission Standards on the Design of Aircraft Gas Turbine Engine Combustors 760909
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.
Citation: Rudey, R., "The Impact of Emission Standards on the Design of Aircraft Gas Turbine Engine Combustors," SAE Technical Paper 760909, 1976, https://doi.org/10.4271/760909. Download Citation
Author(s):
Richard A. Rudey
Pages: 12
Event:
Aerospace Engineering and Manufacturing Meeting
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Engine components
Exhaust emissions
Environmental regulations and standards
Emissions control
Aircraft
Environmental protection
Emissions
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