点火系统
燃烧室
汽油机
汽车工程
点火正时
声学
圆柱
发动机爆震
燃油喷射
喷射(流体)
均质压燃
燃烧
机械
材料科学
内燃机
工程类
机械工程
航空航天工程
物理
化学
有机化学
作者
Muhammed Fayaz Palakunnummal,Sahu Priyadarshi,Mark Ellis,M.A.A. Nazha
出处
期刊:SAE International journal of engines
[SAE International]
日期:2021-02-26
卷期号:14 (3): 405-417
被引量:3
标识
DOI:10.4271/03-14-03-0024
摘要
Pre-chamber ignition system has the potential to reduce burn duration of lean-burn gasoline engine combustion and can achieve reduced knock occurrence from the distributed ignition sources. Pre-chamber ignition produces high velocity turbulent jets and these jets often reach sonic velocity and produce shock waves inside the combustion chamber. These shock waves make knock detection difficult with a conventional surface mounted acoustic knock sensor. This paper discusses how an acoustic knock sensor works with pre-chamber ignition and evaluates different cylinder pressure-based knock detection strategies and proposes a method which eliminates the influence of jet induced oscillations on knock detection.
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