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预燃室结构参数对氨氢发动机燃烧特性的影响

贾国欣 鞠洪玲 李晨龙

内燃机工程2026,Vol.47Issue(3):51-60,10.
内燃机工程2026,Vol.47Issue(3):51-60,10.DOI:10.13949/j.cnki.nrjgc.2026.03.006

预燃室结构参数对氨氢发动机燃烧特性的影响

Effects of Pre-chamber Structural Parameters on the Combustion Characteristics of an Ammonia-Hydrogen Engine

贾国欣 1鞠洪玲 1李晨龙1

作者信息

  • 1. 武汉理工大学汽车工程学院,武汉 430070
  • 折叠

摘要

Abstract

To investigate the influence of pre-chamber geometry on jet ignition performance,a three-dimensional numerical study was conducted on an ammonia-hydrogen active pre-chamber engine using a detailed chemical reaction mechanism.Nine pre-chamber configurations were designed based on an orthogonal experimental method to systematically analyze the effects of throat diameter,jet orifice type,and jet horizontal angle on the combustion process.The results indicate that an excessively small throat diameter reduces jet turbulence intensity and degrades combustion performance,while a divergent jet orifice significantly enhances ignition stability.An appropriate jet horizontal angle effectively strengthens in-cylinder turbulence by utilizing combustion chamber geometry,thereby shortening the late combustion duration,although additional heat transfer losses may occur.Furthermore,a Taguchi-based sensitivity analysis was employed to quantify the relative influence of structural parameters at different combustion stages.During the ignition delay stage,throat diameter and jet orifice type dominate the ignition behavior,accounting for up to 96.27%of the total influence.In the early combustion stage,throat diameter remains the primary controlling factor with a contribution of 51.2%.In the late combustion stage,the jet horizontal angle becomes dominant,contributing 50.37%.For the overall combustion duration,the throat diameter exhibits the highest influence(about 49%),followed by the jet horizontal angle(about 36%),while the jet orifice type plays a comparatively minor role(about 15%).

关键词

氨氢发动机/预燃室结构/射流点火/燃烧相位/信噪比

Key words

ammonia-hydrogen engine/pre-chamber structure/jet ignition/combustion phasing/signal-to-noise ratio

分类

能源科技

引用本文复制引用

贾国欣,鞠洪玲,李晨龙..预燃室结构参数对氨氢发动机燃烧特性的影响[J].内燃机工程,2026,47(3):51-60,10.

基金项目

国家自然科学基金重点项目(51706163)National Natural Science Foundation of China(51706163) (51706163)

内燃机工程

1000-0925

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