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Frontiers in Energy

ISSN 2095-1701

ISSN 2095-1698(Online)

CN 11-6017/TK

Postal Subscription Code 80-972

2018 Impact Factor: 1.701

Front Energ    2012, Vol. 6 Issue (3) : 296-303    https://doi.org/10.1007/s11708-012-0191-0
RESEARCH ARTICLE
Numerical simulation of bituminous coal combustion in a full-scale tiny-oil ignition burner: influence of excess air ratio
Zhengqi LI(), Chunlong LIU, Xiang ZHANG, Lingyan ZENG, Zhichao CHEN
School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
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Abstract

The progression of ignition was numerically simulated with the aim of realizing a full-scale tiny-oil ignition burner that is identical to the burner used in an 800 MWe utility boiler. The numerical simulations were conducted for four excess air ratios, 0.56, 0.75, 0.98 and 1.14 (corresponding to primary air velocities of 17, 23, 30 and 35 m/s, respectively), which were chosen because they had been used previously in practical experiments. The numerical simulations agreed well with the experimental results, which demonstrate the suitability of the model used in the calculations. The gas temperatures were high along the center line of the burner for the four excess air ratios. The flame spread to the burner wall and the high-temperature region was enlarged in the radial direction along the primary air flow direction. The O2 concentrations for the four excess air ratios were 0.5%, 1.1%, 0.9% and 3.0% at the exit of the second combustion chamber. The CO peak concentration was very high with values of 7.9%, 9.9%, 11.3% and 10.6% for the four excess air ratios at the exit of the second combustion chamber.

Keywords numerical simulation      tiny-oil ignition burner      pulverized coal      temperature field     
Corresponding Author(s): LI Zhengqi,Email:green@hit.edu.cn   
Issue Date: 05 September 2012
 Cite this article:   
Chunlong LIU,Xiang ZHANG,Lingyan ZENG, et al. Numerical simulation of bituminous coal combustion in a full-scale tiny-oil ignition burner: influence of excess air ratio[J]. Front Energ, 2012, 6(3): 296-303.
 URL:  
https://academic.hep.com.cn/fie/EN/10.1007/s11708-012-0191-0
https://academic.hep.com.cn/fie/EN/Y2012/V6/I3/296
Fig.1  Experimental setup
Fig.2  Three-dimensional mesh generation
Oil typeDiesel oil
Oil pressure/MPa1.0
Oil flow rate of main oil gun/(kg·h-1)35
Oil flow rate of auxiliary oil gun/(kg·h-1)65
Flow rate of compressed and burned air/(m3·h-1)500
Primary air velocity/(m·s -3)17-35
Primary air temperature/°C15
Coal feed rate/(t·h-1)4
Tab.1  List of the parameters used in this study
Carbon/%Hydrogen/%Sulfur/%Nitrogen/%Oxygen/%
85.3313.290.250.040.66
Ash/%Moisture/%Gross calorific value/(kJ·kg-1)Flash point/°CDensity/(kg·m-3)
0.380.054132062870
Tab.2  Ultimate analysis results and other characteristics of 0# light diesel oil
Proximate analysis (as air dry basis)
Volatile matter/%Ash/%Moisture/%Fixed carbon/%Gross calorific value/(kJ·kg-1)
30.9713.912.8152.3227290
Ultimate analysis (as air dry basis)
Carbon/%Hydrogen/%Sulfur/%Nitrogen/%Oxygen/%
70.103.840.500.927.92
Tab.3  Characteristics of the bituminous pulverized coal used
Fig.3  Comparison of calculated temperature with measured temperature on the center line of the burner for different excess air ratios
Fig.4  Maximum temperatures at various sections along the flow direction of the primary air and the radial positions of the maximum temperatures for different excess air ratios
Fig.5  Gas temperature (°C) distributions in the burner at an excess air ratio of 0.75
Fig.6  Comparison of calculated temperature with measured temperature at the exits of the first and second combustion chambers for different excess air ratios
Fig.7  Comparison of calculated O concentration distribution along the radial direction at the exits of the first and second combustion chambers and measured O concentration at the exits of the second combustion chambers for different excess air ratios
Fig.8  CO concentration distribution along the radial direction at the exit of the second combustion chamber for different excess air ratios
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