Combustion Science and Technology · 1976 · 11 citations · 3 references
EngineeringChemical EngineeringChemistryCatalysisCombustionReaction EngineeringCatalytic Reaction EngineeringCombustion In EnginesCombustion ProcessesEngine PerformanceGas Turbine CombustionGas Turbine EnginesAir-fuel RatioAir-fuel Ratio EffectsCatalytic CombustionControl RequirementsExhaust Gas AnalysisResidence TimeTransient Engine Operation
Abstract Three different catalysts consisting of Pt catalyst coated ceramic monolith having differing catalyst surface concentrations have been utilized to investigate the combustion of CaHg/air mixtures at inlet temperatures of 700–730 °K as a function of CaHs/air ratios. Catalytic combustion is self-initiated at these inlet temperatures even when the fuel/air ratio is quite lean, Analyses of NO, NOx, CO, CO2, and HC in the exhaust gas stream reveal that good conversion of fuel as well as CO to CO2 can occur catalytically without producing excessive NOx. The maximum combustion efficiency achieved was 99·9998% (calculated from combustion inefficiency measurements) at CaHg/air = 0·0152, inlet temperature of 719 K, and a residence time of 12 ms and the emission indexes, g pollutant/kg fuel, of NOx, HC, and CO were 0·042, 0, and 0·222, respectively. Prior to successful product application to gas turbine engines certain significant engineering/design obstacles must be evaluated and/or eliminated, such as cold start, transient operation (control requirements), life time, as well as physical volume requirements.
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Investigation of Aircraft Gas Turbine Combustor Having Low Mass Emissions
D. L. Troth, A.J. Verdouw, John Williams et al. · 1974 · 12 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17