TY - JOUR
T1 - RANS simulations on combustion and emission characteristics of a premixed NH3/H2 swirling flame with reduced chemical kinetic model
AU - SUN, Yuze
AU - CAI, Tao
AU - SHAHSAVARI, Mohammad
AU - SUN, Dakun
AU - SUN, Xiaofeng
AU - ZHAO, Dan
AU - WANG, Bing
N1 - Publisher Copyright:
© 2021 Chinese Society of Aeronautics and Astronautics
PY - 2021/12
Y1 - 2021/12
N2 - Ammonia (NH3) is considered as a potential alternative carbon free fuel to reduce greenhouse gas emission to meet the increasingly stringent emission requirements. Co-burning NH3 and H2 is an effective way to overcome ammonia's relative low burning velocity. In this work, 3D Reynolds Averaged Navier-Stokes (RANS) numerical simulations are conducted on a premixed NH3/H2 swirling flame with reduced chemical kinetic mechanism. The effects of (A) overall equivalence ratio Φ and (B) hydrogen blended molar fraction XH2 on combustion and emission characteristics are examined. The present results show that when 100%NH3-0%H2-air are burnt, the NO emission and unburned NH3 of at the swirling combustor outlet has the opposite varying trends. With the increase of Φ, NO emission is found to be decreased, while the unburnt ammonia emission is increased. NH2 → HNO, NH → HNO and HNO → NO sub-paths are found to play a critical role in NO formation. Normalized reaction rate of all these three sub-paths is shown to be decreased with increased Φ. Hydrogen addition is shown to significantly increase the laminar burning velocity of the mixed fuel. However, adding H2 does not affect the critical equivalence ratio corresponding to the maximum burning velocity. The emission trend of NO and unburnt NH3 with increased Φ is unchanged by blending H2. NO emission with increased XH2 is increased slightly less at a larger Φ than that at a smaller Φ. In addition, reaction rates of NH2 → HNO and HNO → NO sub-paths are decreased with increased XH2, when Φ is larger. Under all tested cases, blending H2 with NH3 reduces the unburned NH3 emission, especially for rich combustion conditions. In summary, the present work provides research finding on supporting applying ammonia with hydrogen blended in low-emission gas turbine engines.
AB - Ammonia (NH3) is considered as a potential alternative carbon free fuel to reduce greenhouse gas emission to meet the increasingly stringent emission requirements. Co-burning NH3 and H2 is an effective way to overcome ammonia's relative low burning velocity. In this work, 3D Reynolds Averaged Navier-Stokes (RANS) numerical simulations are conducted on a premixed NH3/H2 swirling flame with reduced chemical kinetic mechanism. The effects of (A) overall equivalence ratio Φ and (B) hydrogen blended molar fraction XH2 on combustion and emission characteristics are examined. The present results show that when 100%NH3-0%H2-air are burnt, the NO emission and unburned NH3 of at the swirling combustor outlet has the opposite varying trends. With the increase of Φ, NO emission is found to be decreased, while the unburnt ammonia emission is increased. NH2 → HNO, NH → HNO and HNO → NO sub-paths are found to play a critical role in NO formation. Normalized reaction rate of all these three sub-paths is shown to be decreased with increased Φ. Hydrogen addition is shown to significantly increase the laminar burning velocity of the mixed fuel. However, adding H2 does not affect the critical equivalence ratio corresponding to the maximum burning velocity. The emission trend of NO and unburnt NH3 with increased Φ is unchanged by blending H2. NO emission with increased XH2 is increased slightly less at a larger Φ than that at a smaller Φ. In addition, reaction rates of NH2 → HNO and HNO → NO sub-paths are decreased with increased XH2, when Φ is larger. Under all tested cases, blending H2 with NH3 reduces the unburned NH3 emission, especially for rich combustion conditions. In summary, the present work provides research finding on supporting applying ammonia with hydrogen blended in low-emission gas turbine engines.
KW - Ammonia
KW - Emission
KW - Hydrogen
KW - Premixed combustion
KW - Reduced mechanism
KW - Swirling flame
UR - https://www.scopus.com/pages/publications/85107570386
U2 - 10.1016/j.cja.2020.11.017
DO - 10.1016/j.cja.2020.11.017
M3 - 文章
AN - SCOPUS:85107570386
SN - 1000-9361
VL - 34
SP - 17
EP - 27
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 12
ER -