TY - JOUR
T1 - Burning velocity and flame structure of CH 4 /NH 3 /air turbulent premixed flames at high pressure
AU - Ichikawa, Akinori
AU - Naito, Yuji
AU - Hayakawa, Akihiro
AU - Kudo, Taku
AU - Kobayashi, Hideaki
N1 - Funding Information:
This research was supported by the Council for Science, Technology and Innovation (CSTI) , the Cross-ministerial Strategic Innovation Promotion Program(SIP ), “Energy Carriers” (Funding Agency: the Japan Science and Technology Agency (JST)).
Publisher Copyright:
© 2019 Hydrogen Energy Publications LLC
PY - 2019/3/8
Y1 - 2019/3/8
N2 - Ammonia is one of the most promising alternative fuels. In particular, ammonia combustion for gas turbine combustors for power generation is expected. To shift the fuel for a gas turbine combustor to ammonia step-by-step, the partial replacement of natural gas by ammonia is considered. To reveal the turbulent combustion characteristics, CH 4 /NH 3 /air turbulent premixed flame at 0.5 MPa was experimentally investigated. The ammonia ratio based on the mole fraction and lower heating value was varied from 0 to 0.2. The results showed that the ratio of the turbulent burning velocity and unstretched laminar burning velocity decreased with an increase in the ammonia ratio. The reason for this variation is that the flame area decreased with an increase in the ammonia ratio as the flame surface density decreased and the fractal inner cutoff increased. The volume fractions in the turbulent flame region were almost the same with ammonia addition, indicating that combustion oscillation can be handled in a manner similar to that for the case of natural gas for CH 4 /NH 3 /air flames.
AB - Ammonia is one of the most promising alternative fuels. In particular, ammonia combustion for gas turbine combustors for power generation is expected. To shift the fuel for a gas turbine combustor to ammonia step-by-step, the partial replacement of natural gas by ammonia is considered. To reveal the turbulent combustion characteristics, CH 4 /NH 3 /air turbulent premixed flame at 0.5 MPa was experimentally investigated. The ammonia ratio based on the mole fraction and lower heating value was varied from 0 to 0.2. The results showed that the ratio of the turbulent burning velocity and unstretched laminar burning velocity decreased with an increase in the ammonia ratio. The reason for this variation is that the flame area decreased with an increase in the ammonia ratio as the flame surface density decreased and the fractal inner cutoff increased. The volume fractions in the turbulent flame region were almost the same with ammonia addition, indicating that combustion oscillation can be handled in a manner similar to that for the case of natural gas for CH 4 /NH 3 /air flames.
KW - Ammonia
KW - High pressure
KW - Methane
KW - Turbulent burning velocity
KW - Turbulent combustion
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U2 - 10.1016/j.ijhydene.2019.01.193
DO - 10.1016/j.ijhydene.2019.01.193
M3 - Article
AN - SCOPUS:85061584878
SN - 0360-3199
VL - 44
SP - 6991
EP - 6999
JO - International Journal of Hydrogen Energy
JF - International Journal of Hydrogen Energy
IS - 13
ER -