Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 267-273 |
| Number of pages | 7 |
| Journal | Zhongguo Hangkong Taikong Xuehui Huikan/Transactions of the Aeronautical and Astronautical Society of the Republic of China |
| Volume | 34 |
| Issue number | 3 |
| Publication status | Published - 2002 Sept 1 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering