화학공학소재연구정보센터
Catalysis Today, Vol.26, No.3-4, 337-344, 1995
Development of a High-Temperature Combustion Catalyst System and Prototype Catalytic Combustor Turbine Test-Results
A new combustion catalyst system for gas turbines composed of high-temperature durable ceramic catalysts made of fine manganese-substituted hexaaluminate particles and noble metal-carrying cordierite honeycomb catalysts has been developed. A 160 kW prototype catalytic combustor turbine rigged with a 220 mm in diameter catalyst system was constructed and tested including a continuous 215-hour operation and repeated sudden stops. The results showed practical combustion performance with ultra-low NOx emissions less than 40 ppm (converted to 0% oxygen) and the feasibility of long term catalyst durability.