TY - JOUR
T1 - One axial fuel injected vortex-tube combustor with high capacity of combustion stabilization for NOx reduction
AU - Ren, Shoujun
AU - Yang, Haolin
AU - Jiang, Liqiao
AU - Zhao, Daiqing
AU - Wang, Xiaohan
N1 - Publisher Copyright:
© 2020 Elsevier Ltd
PY - 2020/11/15
Y1 - 2020/11/15
N2 - A novel vortex-tube combustor with axial fuel injection for NOx reduction was proposed to overcome the instability of ultra-lean combustion. The stability limit, flame configuration, NOx and CO emissions, and flame structure were investigated experimentally under various global equivalence ratios and fuel flow rates. The mechanisms of NOx emission reduction were analyzed by numerical simulation. Results show that the limit of global equivalence ratio can be as low as 0.01 and the amplitude of pressure fluctuation is always less than 1300 Pa, indicating fairly good performance in combustion stabilization of the combustor. In the operation range, there is a trade-off region with low NOx and CO simultaneously. The diffusion-like flame structure in this combustor can enhance the local equivalence ratio, whilst the flow field structure can also promote the transport of chemical enthalpy to the flame front, thus facilitating the stabilization. The enhanced stabilization enables the ultra-lean combustion and the ensued small area of the high-temperature zone to conduct, as well as the low NOx formation through reducing thermal NO. The local fuel-rich region and the flow field structure can promote the NOx to be reduced further via the Fenimore mechanism.
AB - A novel vortex-tube combustor with axial fuel injection for NOx reduction was proposed to overcome the instability of ultra-lean combustion. The stability limit, flame configuration, NOx and CO emissions, and flame structure were investigated experimentally under various global equivalence ratios and fuel flow rates. The mechanisms of NOx emission reduction were analyzed by numerical simulation. Results show that the limit of global equivalence ratio can be as low as 0.01 and the amplitude of pressure fluctuation is always less than 1300 Pa, indicating fairly good performance in combustion stabilization of the combustor. In the operation range, there is a trade-off region with low NOx and CO simultaneously. The diffusion-like flame structure in this combustor can enhance the local equivalence ratio, whilst the flow field structure can also promote the transport of chemical enthalpy to the flame front, thus facilitating the stabilization. The enhanced stabilization enables the ultra-lean combustion and the ensued small area of the high-temperature zone to conduct, as well as the low NOx formation through reducing thermal NO. The local fuel-rich region and the flow field structure can promote the NOx to be reduced further via the Fenimore mechanism.
KW - Axial fuel injection
KW - Diffusion-like flame
KW - NO emissions
KW - Stability limit
KW - Vortex-tube combustor
UR - https://www.scopus.com/pages/publications/85089943226
U2 - 10.1016/j.energy.2020.118659
DO - 10.1016/j.energy.2020.118659
M3 - Article
AN - SCOPUS:85089943226
SN - 0360-5442
VL - 211
JO - Energy
JF - Energy
M1 - 118659
ER -