Development of a high-temperature combustion catalyst system and prototype catalytic combustor turbine test results

被引:22
作者
Sadamori, H
Tanioka, T
Matsuhisa, T
机构
[1] KOBE STEEL LTD,POLYMER & CHEM TECHNOL RES LAB,KOBE,HYOGO 65122,JAPAN
[2] CATALYSTS & CHEM INC,SHIMONOSEKI FACTORY,SHIMONOSEKI,YAMAGUCHI 750,JAPAN
关键词
combustion; gas turbines; high temperature combustion;
D O I
10.1016/0920-5861(95)00156-8
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
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.
引用
收藏
页码:337 / 344
页数:8
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[3]  
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