In-cylinder in-depth combustion investigation for a heavy-duty diesel engine

IF 5.4 2区 工程技术 Q1 ENGINEERING, AEROSPACE
Anam Ali, Khalid Saifullah Syed
{"title":"In-cylinder in-depth combustion investigation for a heavy-duty diesel engine","authors":"Anam Ali,&nbsp;Khalid Saifullah Syed","doi":"10.1016/j.jppr.2024.09.001","DOIUrl":null,"url":null,"abstract":"<div><div>This present study is part of the design improvement process of a specified high torque low-speed engine. This work aims at carrying out an in-depth analysis of in-cylinder combustion, mesh sensitivity, and engine performance at supercharge conditions to provide a foundation for the design improvement process of the given engine. The computational fluid dynamic (CFD) simulations are carried out on a 3D sector from <span><math><mrow><mo>−</mo><mn>130</mn><mo>°</mo></mrow></math></span> to <span><math><mrow><mrow><mn>130</mn><mo>°</mo></mrow></mrow></math></span> crank angle (CA) by employing appropriate models to represent the different physical and chemical processes and using the finite volume method for solving the governing differential equations. An extensive investigation has been carried out for the choice of base mesh size and the number of local and temporal refinements to capture the phenomena happening in the combustion chamber at diverse temporal and local scales. The present results have been validated against available literature experimental and simulation results. Primary field variables and the well-known four phases of combustion have been studied for gaining in-depth insight into these phenomena. Cylinder average pressure, mean temperature, heat release rate (HRR), integrated heat release rate (IHRR), and emissions of <span><math><mrow><msub><mtext>CO</mtext><mn>2</mn></msub></mrow></math></span>, CO, <span><math><mrow><msub><mtext>NO</mtext><mi>x</mi></msub></mrow></math></span>, HC and soot are presented to assess the quality of combustion. Engine performance analysis has been done in terms of combustion efficiency, gross work, power, torque, and integrated mean effective pressure (IMEP). The base mesh of 1.4 mm may be an appropriate choice during the injection and combustion process spanning throughout around <span><math><mrow><mrow><mn>40</mn><mo>°</mo></mrow></mrow></math></span> CA from the start of injection while in the remaining simulation duration of around <span><math><mrow><mrow><mn>220</mn><mo>°</mo></mrow></mrow></math></span> CA base mesh of 2 mm gives a sufficient resolution. It has been found that maximum heat release takes place in Phase-III, the mixing-controlled phase, of the combustion process. More than 98% combustion efficiency has been achieved in all the simulations. Around 99% of the total heat release and emissions production takes place within <span><math><mrow><mrow><mn>60</mn><mo>°</mo></mrow></mrow></math></span> CA after top dead center (ATDC).</div></div>","PeriodicalId":51341,"journal":{"name":"Propulsion and Power Research","volume":"13 3","pages":"Pages 335-359"},"PeriodicalIF":5.4000,"publicationDate":"2024-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Propulsion and Power Research","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2212540X24000555","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

This present study is part of the design improvement process of a specified high torque low-speed engine. This work aims at carrying out an in-depth analysis of in-cylinder combustion, mesh sensitivity, and engine performance at supercharge conditions to provide a foundation for the design improvement process of the given engine. The computational fluid dynamic (CFD) simulations are carried out on a 3D sector from 130° to 130° crank angle (CA) by employing appropriate models to represent the different physical and chemical processes and using the finite volume method for solving the governing differential equations. An extensive investigation has been carried out for the choice of base mesh size and the number of local and temporal refinements to capture the phenomena happening in the combustion chamber at diverse temporal and local scales. The present results have been validated against available literature experimental and simulation results. Primary field variables and the well-known four phases of combustion have been studied for gaining in-depth insight into these phenomena. Cylinder average pressure, mean temperature, heat release rate (HRR), integrated heat release rate (IHRR), and emissions of CO2, CO, NOx, HC and soot are presented to assess the quality of combustion. Engine performance analysis has been done in terms of combustion efficiency, gross work, power, torque, and integrated mean effective pressure (IMEP). The base mesh of 1.4 mm may be an appropriate choice during the injection and combustion process spanning throughout around 40° CA from the start of injection while in the remaining simulation duration of around 220° CA base mesh of 2 mm gives a sufficient resolution. It has been found that maximum heat release takes place in Phase-III, the mixing-controlled phase, of the combustion process. More than 98% combustion efficiency has been achieved in all the simulations. Around 99% of the total heat release and emissions production takes place within 60° CA after top dead center (ATDC).
重型柴油发动机缸内深度燃烧研究
本研究是特定高扭矩低速发动机设计改进过程的一部分。这项工作旨在对增压条件下的缸内燃烧、网格敏感性和发动机性能进行深入分析,为特定发动机的设计改进过程奠定基础。通过采用适当的模型来表示不同的物理和化学过程,并使用有限体积法来求解控制微分方程,对曲柄角(CA)从 -130° 到 130° 的三维扇形区域进行了计算流体动力学(CFD)模拟。对基础网格大小的选择以及局部和时间细化的数量进行了广泛的研究,以捕捉燃烧室内不同时间和局部尺度上发生的现象。目前的结果已根据现有的文献实验和模拟结果进行了验证。为了深入了解这些现象,对主要的现场变量和众所周知的燃烧四阶段进行了研究。气缸平均压力、平均温度、热释放率 (HRR)、综合热释放率 (IHRR) 以及二氧化碳、一氧化碳、氮氧化物、碳氢化合物和烟尘的排放情况都被列出,以评估燃烧质量。发动机性能分析包括燃烧效率、总功、功率、扭矩和综合平均有效压力(IMEP)。在喷射和燃烧过程中,1.4 毫米的基本网格可能是一个合适的选择,从喷射开始,网格跨度约为 40° CA,而在其余约 220° CA 的模拟持续时间内,2 毫米的基本网格提供了足够的分辨率。研究发现,最大热量释放发生在燃烧过程的第三阶段,即混合控制阶段。所有模拟的燃烧效率都超过了 98%。约 99% 的总热量释放和排放产生于顶死中心 (ATDC) 后 60° CA 范围内。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
CiteScore
7.50
自引率
5.70%
发文量
30
期刊介绍: Propulsion and Power Research is a peer reviewed scientific journal in English established in 2012. The Journals publishes high quality original research articles and general reviews in fundamental research aspects of aeronautics/astronautics propulsion and power engineering, including, but not limited to, system, fluid mechanics, heat transfer, combustion, vibration and acoustics, solid mechanics and dynamics, control and so on. The journal serves as a platform for academic exchange by experts, scholars and researchers in these fields.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信