Numerical and experimental study of the effects of fuel injection and equivalence ratio in a can micro-combustor at atmospheric condition

被引:9
|
作者
Sadatakhavi, SeyedMohammadReza [1 ]
Tabejamaat, Sadegh [1 ]
EiddiAttarZade, Masoud [1 ]
Kankashvar, Benyamin [1 ]
Nozari, MohammadReza [1 ]
机构
[1] AmirKabir Univ Technol, Dept Aerosp Engn, Hafez Ave, Tehran, Iran
关键词
Can Micro-combustor; Atmospheric condition; Experimental and numerical investigation; Equivalence ratio; Injection pressure; Reactive characteristics; EMISSION CHARACTERISTICS;
D O I
10.1016/j.energy.2021.120166
中图分类号
O414.1 [热力学];
学科分类号
摘要
The present paper aims to examine experimentally and numerically the effect of equivalence ratio and injection pressure on combustion in a can combustor. The results show the combustor temperature rises with an increase in the overall equivalence ratio. With an increase in the injection pressure at a constant equivalence ratio, the flame is extended to the combustor downstream. The IRZ (Inner Recirculation Zone) region in the primary zone has high turbulence kinetic energy increasing the fuel droplet evaporation rate. This zone provides a region of appropriate mixing of fuel-air, leading to a zone of flame holding. In the intermediate zone, the mixture fraction near liner walls reaches its stoichiometric value, and a flame is formed near the liner walls. With an increase in the equivalence ratio or injection pressure at constant equivalence ratio, the incomplete combustion species is reduced and the pattern factor and combustion efficiency are improved. (c) 2021 Elsevier Ltd. All rights reserved.
引用
收藏
页数:12
相关论文
共 50 条
  • [1] Experimental and numerical study of combustion characteristics in a liquid fuel CAN micro-combustor
    SadatAkhavi, SeyedMohammadReza
    Tabejamaat, Sadegh
    EiddiAttarZade, Masoud
    Kankashvar, Benyamin
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 105
  • [2] NUMERICAL AND EXPERIMENTAL STUDY ON SOOT ACCUMULATION ON THE WALL OF FALLING FUEL FILM MICRO-COMBUSTOR
    Mei, Ning
    Wang, Xiaoyan
    Zhao, Hongming
    Li, Yan
    Si, Hongyu
    [J]. PROCEEDINGS OF THE ASME INTERNATIONAL HEAT TRANSFER CONFERENCE - 2010 , VOL 3: COMBUSTION, CONDUCTION, ELECTRONIC COOLING, EVAPORATION,TWO-PHASE FLOW, 2010, : 13 - 18
  • [3] Numerical study on heat recirculation in a porous micro-combustor
    Li, Jun
    Li, Qingqing
    Shi, Junrui
    Liu, Xueling
    Guo, Zhaoli
    [J]. COMBUSTION AND FLAME, 2016, 171 : 152 - 161
  • [4] Experimental study on falling-film micro-combustor
    Si, Hong-Yu
    Mei, Ning
    Wang, Xiao-Yan
    Zhao, Hong-Ming
    Ding, Shuang
    [J]. Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2010, 31 (12): : 2159 - 2162
  • [5] Experimental study of the effect of the spray cone angle on the temperature distribution in a can micro-combustor
    Kankashvar, Benyamin
    Tabejamaat, Sadegh
    EidiAttarZade, Masoud
    Sadatakhavi, Seyed MohammadReza
    Nozari, Mohammadreza
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 115
  • [6] Experimental study of equivalence ratio and fuel flow rate effects on nonlinear thermoacoustic instability in a swirl combustor
    Zhao, He
    Li, Guoneng
    Zhao, Dan
    Zhang, Zhiguo
    Sun, Dakun
    Yang, Wenming
    Li, Shen
    Lu, Zhengli
    Zheng, Youqu
    [J]. APPLIED ENERGY, 2017, 208 : 123 - 131
  • [7] Experimental study on effects of fuel injection on scramjet combustor performance
    Wu Xianyu
    Li Xiaoshan
    Ding Meng
    Liu Weidong
    Wang Zhenguo
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2007, 20 (06) : 488 - 494
  • [8] Experimental study on effects of fuel injection on scramjet combustor performance
    Wu, Xianyu
    Li, Xiaoshan
    Ding, Meng
    Liu, Weidong
    Wang, Zhenguo
    [J]. Chinese Journal of Aeronautics, 2007, 20 (06): : 488 - 494
  • [10] Thermodynamic Study of the Humidity Ratio for Methane Reforming at Low Temperature in a Micro-Combustor
    Zhao Liu-Jie
    Ran Jing-Yu
    Wu Sheng
    [J]. ACTA PHYSICO-CHIMICA SINICA, 2011, 27 (09) : 2027 - 2034