Effect of bioethanol on combustion and emissions in advanced CI engines: HCCI, PPC and GCI mode - A review

被引:91
作者
Noh, Hyun Kwon [1 ]
No, Soo-Young [1 ]
机构
[1] Chungbuk Natl Univ, Dept Biosyst Engn, Cheongju 28644, South Korea
基金
美国国家科学基金会;
关键词
Bioethanol; Advanced CI engines; Homogeneous charge compression ignition; Partially premixed; Combustion; Gasoline compression ignition; LOW-TEMPERATURE COMBUSTION; COMPRESSION-IGNITION COMBUSTION; DIESEL FUEL BLENDS; OPERATING-CONDITIONS; CONVENTIONAL DIESEL; EXHAUST EMISSIONS; FORCED INDUCTION; DIETHYL-ETHER; HEAT RELEASE; WET ETHANOL;
D O I
10.1016/j.apenergy.2017.09.071
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
This review mainly concerns the use of bioethanol in advanced compression ignition (CI) engines. Various advanced CI engines are in existence, and this review discusses, homogeneous charge compression ignition (HCCI) combustion, partially premixed combustion (PPC) and gasoline compression ignition (GCI) combustion for discussion. Four different experimental configurations were adopted to measure the autoignition or ignition delay time for ethanol in HCCI combustion mode. The mixture formation strategies in bioethanol HCCI combustion can be categorized into three groups: external, internal and combined mixture preparations. The external mixture preparation is subdivided into port fuel injection and a vaporizer, and the internal mixture preparation into early, late and multiple direct injections. A numerical simulation for ethanol HCCI combustion was recently carried out with a direct numerical simulation and large eddy simulation. The different reduced chemical kinetic mechanisms for ethanol oxidation models present in the literature are summarized in detail. Detailed mechanisms including 57 species and 383 reactions were employed in numerical simulations of ethanol HCCI combustion. The pressure rise rate, ringing intensity and noise meter calculation for the knock limit and coefficient of variation of indicated mean effective pressure for misfire limit were used. The pressure rise rate has been extensively adopted for the upper limit of the HCCI and PPC combustion, and the acceptable limit for the maximum pressure rise rate is found to be subjective. Studies related to PPC and GCI modes fueled with ethanol makes use of fueling configuration that are divided into single and double injections. A double injection strategy was preferred for ethanol PPC with a combination of 50% EGR and relative equivalence ratio of 0.67. The review of the literature on ethanol PPC and ECI provides an overview of the fueling configuration. Further studies on GCI combustion with ethanol, i.e. ethanol-fueled compression ignition (ECI) are required in the future. In all advanced combustion modes, NOx and soot emissions are low compared to those of conventional diesel engines, and HC and CO emissions are still high in all advanced combustion concepts.
引用
收藏
页码:782 / 802
页数:21
相关论文
共 141 条
[1]  
Acevedo H, 2012, PROCEEDINGS OF THE ASME INTERNAL COMBUSTION ENGINE DIVISION FALL TECHNICAL CONFERENCE - 2012, P393
[2]  
Aceves SM, 2003, 2003011814 SAE
[3]   Combustion advancements in gasoline engines [J].
Alkidas, Alex C. .
ENERGY CONVERSION AND MANAGEMENT, 2007, 48 (11) :2751-2761
[4]  
Andreae M. M., 2007, 2007011858 SAE
[5]  
[Anonymous], 2014011304 SAE
[6]  
[Anonymous], 2007, 2007011867 SAE
[7]   Implementation Challenges and Solutions for Homogeneous Charge Compression Ignition Combustion in Diesel Engines [J].
Asad, Usman ;
Zheng, Ming ;
Ting, David S. -K. ;
Tjong, Jimi .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2015, 137 (10)
[8]   Lean homogenous combustion of E-diesel using external mixture formation technique [J].
Avinash, A. ;
Natarajan, S. ;
Mahalakshmi, N. V. .
ALEXANDRIA ENGINEERING JOURNAL, 2015, 54 (03) :271-279
[9]   Challenges and opportunities in improving the production of bio-ethanol [J].
Baeyens, Jan ;
Kang, Qian ;
Appels, Lise ;
Dewil, Raf ;
Lv, Yongqin ;
Tan, Tianwei .
PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2015, 47 :60-88
[10]  
Bahri B., 2013, INT J MECH AEROSP IN, V7, P438