期刊文献+
共找到4篇文章
< 1 >
每页显示 20 50 100
Control of peak pressures of an HCCI engine under varying swirl and operating parameters 被引量:1
1
作者 T. KARTHIKEYA SHARMA G. AMBA PRASAD RAO K. MADHU MURTHY 《Frontiers in Energy》 SCIE CSCD 2016年第3期337-346,共10页
The major advantages of homogeneous charge compression ignition (HCCI) are high efficiency in combination with low NOx-emissions. However, one of the major challenges with HCCI is the control of higher peak pressure... The major advantages of homogeneous charge compression ignition (HCCI) are high efficiency in combination with low NOx-emissions. However, one of the major challenges with HCCI is the control of higher peak pressures which may damage the engine, limiting the HCCI engine life period. In this paper, an attempt is made to analyze computationally the effect of induction swirl in controlling the peak pressures of an HCCI engine under various operating parameters. A single cylinder 1.6 L reentrant piston bowl diesel engine is chosen. For computational analysis, the ECFM-3Z model of STAR - CD is considered because it is suitable for analyzing the combustion processes in SI and CI engines. As an HCCI engine is a hybrid version of SI and CI engines, the ECFM- 3Z model with necessary modifications is used to analyze the peak pressures inside the combustion chamber. The ECFM-3Z model for HCCI mode of combustion is validated with the existing literature to make sure that the results obtained are accurate. Numerical experiments are performed to study the effect of varying properties like speed of the engine, piston bowl geometry, exhaust gas recirculation (EGR) and equivalence ratio under different swirl ratios in controlling the peak pressures inside the combustion chamber. The results show that the swirl ratio has a considerable impact on controlling the peak pressures of HCCI engine. A reduction in peak pressures are observed with a swirl ratio of 4 because of reduced in cylinder temperatures. The combined effect of four operating parameters, i.e., the speed of the engine, piston bowl geometry, EGR, and equivalence ratio with swirl ratios suggest that lower intake temperatures, reentrant piston bowl, higher engine speeds and higher swirl ratios are favorable in controlling the peak pressures. 展开更多
关键词 HCCI engine ecfm-3Z Swirl ratio peak pressures engine speed piston bowl geometry
原文传递
Numerical investigations on HCCI engine with increased induction induced swirl and engine speed 被引量:1
2
作者 T.Karthikeya Sharma G.Amba Prasad Rao K.Madhu Murthy 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第10期3837-3848,共12页
Homogeneous charge compression ignition(HCCI) mode of combustion is popularly known for achieving simultaneous reduction of NOx as well as soot emissions as it combines the compression ignition(CI) and spark ignition(... Homogeneous charge compression ignition(HCCI) mode of combustion is popularly known for achieving simultaneous reduction of NOx as well as soot emissions as it combines the compression ignition(CI) and spark ignition(SI) engine features. In this work, a CI engine was simulated to work in HCCI mode and was analyzed to study the effect of induction induced swirl under varying speeds using three-zone extended coherent flame combustion model(ECFM-3Z, compression ignition) of STAR-CD. The analysis was done considering speed ranging from 800 to 1600 r/min and swirl ratios from 1 to 4. The present study reveals that ECFM-3Z model has well predicted the performance and emissions of CI engine in HCCI mode. The simulation predicts reduced in-cylinder pressures, temperatures, wall heat transfer losses, and piston work with increase in swirl ratio irrespective of engine speed. Also, simultaneous reduction in CO2 and NOx emissions is realized with higher engine speeds and swirl ratios. Low speeds and swirl ratios are favorable for low CO2 emissions. It is observed that increase in engine speed causes a marginal reduction in in-cylinder pressures and temperatures. Also, higher turbulent energy and velocity magnitude levels are obtained with increase in swirl ratio, indicating efficient combustion necessitating no modifications in combustion chamber design. The investigations reveal a total decrease of 38.68% in CO2 emissions and 12.93% in NOx emissions when the engine speed increases from 800 to 1600 r/min at swirl ratio of 4. Also an increase of 14.16% in net work done is obtained with engine speed increasing from 800 to 1600 r/min at swirl ratio of 1. The simulation indicates that there is a tradeoff observed between the emissions and piston work. It is finally concluded that the HCCI combustion can be regarded as low temperature combustion as there is significant decrease in in-cylinder temperatures and pressures at higher speeds and higher swirl ratios. 展开更多
关键词 HCCI engine ecfm-3Z swirl ratio emissions and performance
下载PDF
新型燃烧模型在柴油机燃烧模拟中的应用(上)
3
作者 夏兴兰 杨海涛 +2 位作者 郭立新 缪雪龙 王先勇 《现代车用动力》 2011年第2期1-5,51,共6页
将每个计算单元分为燃料区、空气区和混合区3个区域,在火焰传播方向上又将每个区域分为已燃区和未燃区,建立了柴油机的三区相关火焰燃烧模型,利用该模型对超多喷孔柴油机和传统柴油机缸内燃烧过程进行三维数值模拟,不仅得到了与试验值... 将每个计算单元分为燃料区、空气区和混合区3个区域,在火焰传播方向上又将每个区域分为已燃区和未燃区,建立了柴油机的三区相关火焰燃烧模型,利用该模型对超多喷孔柴油机和传统柴油机缸内燃烧过程进行三维数值模拟,不仅得到了与试验值相符的气缸压力、NOx和SOOT排放量等结果,而且获得了柴油机缸内混合气的浓度场、温度场、NOx质量分数、SOOT质量分数分布等三维结果,三维结果很好地解释了超多喷孔柴油机的低排放的形成机理。 展开更多
关键词 柴油机 燃烧 数值模拟 三区相关火焰模型
下载PDF
新型燃烧模型在柴油机燃烧模拟中的应用(下)
4
作者 夏兴兰 杨海涛 +2 位作者 郭立新 缪雪龙 王先勇 《现代车用动力》 2011年第3期1-4,共4页
将每个计算单元分为燃料区、空气区和混合区3个区域,在火焰传播方向上又将每个区域分为已燃区和未燃区,建立了柴油机的三区相关火焰燃烧模型,利用该模型对超多喷孔柴油机和传统柴油机缸内燃烧过程进行三维数值模拟,不仅得到了与试验值... 将每个计算单元分为燃料区、空气区和混合区3个区域,在火焰传播方向上又将每个区域分为已燃区和未燃区,建立了柴油机的三区相关火焰燃烧模型,利用该模型对超多喷孔柴油机和传统柴油机缸内燃烧过程进行三维数值模拟,不仅得到了与试验值相符的气缸压力、NOx和SOOT排放量等结果,而且获得了柴油机缸内混合气的浓度场、温度场、NOx质量分数、SOOT质量分数分布等三维结果,三维结果很好地解释了超多喷孔柴油机的低排放的形成机理。 展开更多
关键词 柴油机 燃烧 数值模拟 三区相关火焰模型
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部