Abstract
A single annular lean-burn internally-staged combustor consists of pilot stage and main stage. The pilot stage is located in the center-line of the combustion chamber while the main stage surrounds coaxially the pilot stage. There exists a physical isolation called step height between the two stages. The emission tests using a single module rectangular combustor were operated under the idle condition to study the effects of step height on NOX. The commercial software Fluent was used to simulate the cold flow field and combustion performance. The results indicate that step height has a great influence on the emission of NOX. When the step height increases by 38%, the surface and volume of primary center recirculation zone will increase by 6.7% and 16.4%. However, the axial length has a decrease of the small amount and the emission of EINOX will increase by 35.1%.
| Original language | English |
|---|---|
| Pages (from-to) | 941-949 |
| Number of pages | 9 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 35 |
| Issue number | 7 |
| DOIs | |
| State | Published - Jul 2014 |
Keywords
- Aero-engine
- Internally-staged combustor
- Numerical simulation
- Step height
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