共 58 条
Investigation on the combustion performance enhancement of the premixed methane/air in a two-step micro combustor
被引:41
作者:
E, Jiaqiang
[1
,2
,3
]
Liu, Haojie
[1
]
Zhao, Xiaohuan
[1
,2
]
Han, Dandan
[1
,2
]
Peng, Qingguo
[1
,3
]
Zuo, Wei
[1
,2
,3
]
Meng, Tian
[1
,2
]
Qiu, Runzhi
[1
,2
]
机构:
[1] Hunan Univ, State Key Lab Adv Design & Mfg Vehicle Body, Changsha 410082, Hunan, Peoples R China
[2] Hunan Univ, Coll Mech & Vehicle Engn, Changsha 410082, Hunan, Peoples R China
[3] Hunan Univ, Inst New Energy & Energy Saving & Emiss Reduct Te, Changsha 410082, Hunan, Peoples R China
基金:
中国国家自然科学基金;
关键词:
Methane;
Micro combustion;
Effect factors;
Field synergetic analysis;
Performance enhancement;
HEAT RECIRCULATING COMBUSTOR;
ENTROPY GENERATION ANALYSIS;
THERMAL PERFORMANCE;
NUMERICAL INVESTIGATIONS;
THERMOPHOTOVOLTAIC SYSTEM;
POROUS-MEDIA;
CYLINDRICAL COMBUSTOR;
WALL THICKNESS;
HYDROGEN-AIR;
GAS-TURBINE;
D O I:
10.1016/j.applthermaleng.2018.05.101
中图分类号:
O414.1 [热力学];
学科分类号:
摘要:
After a two-step global reaction mechanism is used to compute the chemical reactions of the reacting flows, a premixed methane/air combustion model of a two-step micro combustor is established based on some effect factors such as step angle, wall materials and inlet velocity. Moreover, the three or four kinds of the micro two-step combustors are used to investigate the effect of flame shape in the micro-channel, temperature characteristic, velocity field on the premixed methane combustion and field synergetic degree of the premixed methane/air combustion. It's shown that a suitable step angle and inlet velocity are very useful for enhancing the stability of methane premixed combustion of the two-step micro combustor, and the methane premixed combustion of the two-step micro combustor is also influenced by the wall matericals. Average temperatures of the outlet and combustion efficiencies of the two-step micro combustor at different inlet velocities are verified by the measurement results. It's shown that there are good comprehensive performance and higher synergy degree of the two-step micro combustor at the inlet velocities of 2 m/s and 4 m/s, and there are more and more obvious differences between combustion efficiency after field synergy and original combustion efficiency when the inlet velocities are increased.
引用
收藏
页码:114 / 125
页数:12
相关论文