WHAT CAUSES SLOWER FLAME PROPAGATION IN THE LEAN-COMBUSTION ENGINE

被引:7
作者
KUO, TW
机构
[1] Engine Research Department, General Motors Research Laboratories, Warren, MI
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 1990年 / 112卷 / 03期
关键词
D O I
10.1115/1.2906502
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Previous engine data suggest that slower flame propagation in lean-burn engines could be due to slower flame expansion velocity at lean conditions than at stoichiometric combustion. Two classes of model, a quasi-dimensional enginesimulation program and a multidimensional engine-flow and combustion code, were T.-W. Kuo used to study this effect in detail and to assess the capabilities of the models to Engine Research Department, resolve combustion details. The computed flame-speed data from each program dif- General Motors Research Laboratories! fered somewhat in magnitude, but the predicted trends at various equivalence ratios Warren, Ml 48090 were quite similar. The trends include: (1) The peak in-cyUnder burned-gas temperature decreases by about 300 K as the equivalence ratio is decreased from 0.98 to 0.70. (2) Both the laminar flame speed and the flame-propagation speed, the latter computed from the time derivative of flame radius, decrease with decreasing equivalence ratio. (3) The turbulent burning speed, defined as the ratio of specific fuel-burning rate to the product of the flame frontal area and unburned-mixture density, is relatively insensitive to equivalence-ratio variations at the same flameradius position. The previous experimental finding that the reduction in flamepropagation speed with decreasing equivalence ratio is caused mainly by the lower thermal-expansion speed, calculated by subtracting the turbulent burning speed from the flame-propagation speed, was confirmed. This is a consequence of lower burned-gas temperature for the lean case. Regarding the reliability of the models to resolve the combustion details, limitations of the models are identified and discussed in detail. © 1990 by ASME.
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页码:348 / 356
页数:9
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