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
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