TY - JOUR
T1 - Investigation of the performance characteristics of a miniature catalytic gas turbine combustor
AU - Chao, Yei Chin
AU - Chen, Guan Bang
AU - Tsai, Min Huan
PY - 2002/9/1
Y1 - 2002/9/1
N2 - Catalytically stabilized combustion concept is applied to the design of a miniature gas turbine combustor to stabilize the overall-lean combustion (reaction) in the combustor with the expectation that the problems of NOX/CO pollutions, hot spots and ill pattern factors can be effectively alleviated and the high-temperature durability and reliability of the catalyst can also be effectively improved. In this work, noble metal, Pt honeycomb catalyst is used to stabilize the ultra-lean propane-air combustion. Experimental parameters such as fuel-air ratio, flow velocity, catalyst size, and pressure ratio are varied to gain more insight into the catalytic gas-turbine combustor performance. Results of the performance tests show that the miniature catalytic gas turbine combustor of the current design has several advantages: higher combustor efficiency, lower NOX pollution emission, and more uniform outlet temperature profile with better pattern factor over the original engine of traditional combustor design.
AB - Catalytically stabilized combustion concept is applied to the design of a miniature gas turbine combustor to stabilize the overall-lean combustion (reaction) in the combustor with the expectation that the problems of NOX/CO pollutions, hot spots and ill pattern factors can be effectively alleviated and the high-temperature durability and reliability of the catalyst can also be effectively improved. In this work, noble metal, Pt honeycomb catalyst is used to stabilize the ultra-lean propane-air combustion. Experimental parameters such as fuel-air ratio, flow velocity, catalyst size, and pressure ratio are varied to gain more insight into the catalytic gas-turbine combustor performance. Results of the performance tests show that the miniature catalytic gas turbine combustor of the current design has several advantages: higher combustor efficiency, lower NOX pollution emission, and more uniform outlet temperature profile with better pattern factor over the original engine of traditional combustor design.
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M3 - Article
AN - SCOPUS:0037492499
SN - 1022-0666
VL - 34
SP - 267
EP - 273
JO - Zhongguo Hangkong Taikong Xuehui Huikan/Transactions of the Aeronautical and Astronautical Society of the Republic of China
JF - Zhongguo Hangkong Taikong Xuehui Huikan/Transactions of the Aeronautical and Astronautical Society of the Republic of China
IS - 3
ER -