Toward the Development of an NH3-RRQL System—Part II: Effects of the Primary Combustion Zone Length and Secondary Stage Number of Holes on Stability and EmissionsSource: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:007::page 39Author:Avila Jimenez, Cristian D.
,
Cole, Renee
,
Noble, David R.
,
Steele, Robert
,
Wu, David
,
Emerson, Benjamin
,
Lieuwen, Tim
DOI: 10.1115/1.4069538Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Abstract. Staged combustion systems like the rich–relaxation–quench–lean (RRQL) offer the potential for low nitrogen oxides (NOx) emissions while burning ammonia (NH3). This process involves rich premixed NH3–air combustion in a primary zone, allowing time for NOx relaxation, followed by a lean secondary combustion zone via air injection. However, improper design of the secondary stage can lead to high NOx and nitrous oxide (N2O) emissions, offsetting the climate benefits of carbon-free fuels. This study investigates the effects of primary zone length and secondary stage geometry on the stability and emissions of a lab-scale RRQL system. Experiments were conducted at atmospheric pressure using a modular axial swirl burner (swirl number = 1.1, 16 vanes), with primary equivalence ratios (ϕprimary) of 1.13, 1.15, and 1.18. Two quartz lengths (76 and 178 mm) were tested using a five holes (2.03 mm) secondary injection design. Strong flame interaction and elevated NOx were observed for the 76 mm liner. A longer chamber allowed better NOx relaxation and NH3 cracking. Additional tests with 5-, 10-, and 16-holes configurations showed that fewer holes, implying higher momentum flux ratios, yielded lower NOx–N2O emissions, especially at ϕprimary = 1.13. These effects diminished as ϕprimary decreased from 1.18 down to the optimum 1.13. Diffusion-like combustion was seen for 0.90 ≤ ϕglobal ≤ 1.10, leading to inefficient combustion marked by excess O2 values compared with equilibrium. Optimal performance was achieved with ϕprimary = 1.13 and 0.70 ≤ ϕglobal ≤ 0.90, with estimated burner outlet temperatures between 1720 and 1970 K.
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| contributor author | Avila Jimenez, Cristian D. | |
| contributor author | Cole, Renee | |
| contributor author | Noble, David R. | |
| contributor author | Steele, Robert | |
| contributor author | Wu, David | |
| contributor author | Emerson, Benjamin | |
| contributor author | Lieuwen, Tim | |
| date accessioned | 2026-08-23T07:16:29Z | |
| date available | 2026-08-23T07:16:29Z | |
| date copyright | 2026/07/01 | |
| date issued | 2026 | |
| identifier issn | 0742-4795 | |
| identifier other | gtp-25-1280.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314873 | |
| description abstract | Abstract. Staged combustion systems like the rich–relaxation–quench–lean (RRQL) offer the potential for low nitrogen oxides (NOx) emissions while burning ammonia (NH3). This process involves rich premixed NH3–air combustion in a primary zone, allowing time for NOx relaxation, followed by a lean secondary combustion zone via air injection. However, improper design of the secondary stage can lead to high NOx and nitrous oxide (N2O) emissions, offsetting the climate benefits of carbon-free fuels. This study investigates the effects of primary zone length and secondary stage geometry on the stability and emissions of a lab-scale RRQL system. Experiments were conducted at atmospheric pressure using a modular axial swirl burner (swirl number = 1.1, 16 vanes), with primary equivalence ratios (ϕprimary) of 1.13, 1.15, and 1.18. Two quartz lengths (76 and 178 mm) were tested using a five holes (2.03 mm) secondary injection design. Strong flame interaction and elevated NOx were observed for the 76 mm liner. A longer chamber allowed better NOx relaxation and NH3 cracking. Additional tests with 5-, 10-, and 16-holes configurations showed that fewer holes, implying higher momentum flux ratios, yielded lower NOx–N2O emissions, especially at ϕprimary = 1.13. These effects diminished as ϕprimary decreased from 1.18 down to the optimum 1.13. Diffusion-like combustion was seen for 0.90 ≤ ϕglobal ≤ 1.10, leading to inefficient combustion marked by excess O2 values compared with equilibrium. Optimal performance was achieved with ϕprimary = 1.13 and 0.70 ≤ ϕglobal ≤ 0.90, with estimated burner outlet temperatures between 1720 and 1970 K. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Toward the Development of an NH3-RRQL System—Part II: Effects of the Primary Combustion Zone Length and Secondary Stage Number of Holes on Stability and Emissions | |
| type | Journal Paper | |
| journal volume | 148 | |
| journal issue | 7 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4069538 | |
| journal fristpage | 39 | |
| journal lastpage | 44 | |
| page | 6 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:007 | |
| contenttype | Fulltext |