吉林大学学报(工学版) ›› 2025, Vol. 55 ›› Issue (12): 3804-3813.doi: 10.13229/j.cnki.jdxbgxb.20240533

• 车辆工程·机械工程 • 上一篇    

预燃室内氢喷射参数对氨内燃机燃烧的影响

张孚1(),陈海娥1,李骏1,2,胡昱3,王磊1   

  1. 1.国家能源氢能及氨氢融合新能源技术重点实验室,佛山仙湖实验室,广东 佛山 528200
    2.清华大学 车辆与运载学院,北京 100091
    3.武汉理工大学 汽车学院,武汉 430070
  • 收稿日期:2024-06-20 出版日期:2025-12-01 发布日期:2026-02-03
  • 作者简介:张孚(1991-),男,工程师,硕士.研究方向:发动机及清洁能源燃烧.E-mail:zhangfu@xhlab.cn
  • 基金资助:
    国家自然科学基金项目(T2241003)

Influence of hydrogen injection parameters in pre⁃chamber on combustion characteristics of ammonia fueled internal combustion engines

Fu ZHANG1(),Hai-e CHEN1,Jun LI1,2,Yu HU3,Lei WANG1   

  1. 1.Foshan Xianhu Laboratory,National Energy Key Laboratory for New Hydrogen-Ammonia Energy Technologies,Foshan 528200,China
    2.School of Vehicle and Mobility,Tsinghua University,Beijing 100091,China
    3.School of Automotive Engineering,Wuhan University of Technology,Wuhan 430070,China
  • Received:2024-06-20 Online:2025-12-01 Published:2026-02-03

摘要:

基于1台排量2.2 L且配置主动预燃室的氨燃料内燃机,以氢气作为引燃燃料,采用数值模拟方法分析了不同氢气喷射参数对燃烧性能的影响。结果表明:与喷射脉宽相比,氢气喷射压力和喷射结束时刻对燃烧性能的影响更大,尤其是在燃烧持续期的CA10-CA50阶段。本文研究成果可为氨氢内燃机喷射策略的设计提供参考。

关键词: 氨内燃机, 主动预燃室, 氢气喷射, 喷射参数

Abstract:

Based on a 2.2 L ammonia-fueled internal combustion engine equipped with an active pre-chamber, hydrogen was used as the pilot fuel, and the effects of different hydrogen injection parameters on combustion performance were analyzed via numerical simulation. The results indicate that compared with injection pulse width, hydrogen injection pressure and injection end timing have a more significant impact on combustion performance, particularly during the CA10-CA50 phase of the combustion duration. The research findings can provide a reference for the design of injection strategies for ammonia-hydrogen internal combustion engines.

Key words: ammonia internal combustion engine, active pre-chamber, hydrogen injection, injection parameters

中图分类号: 

  • TK431

表1

发动机规格"

参数数值
排量/L2.2
缸径/mm130
行程/mm166
进气门开启角度/°CA ATDC-377
进气门关闭角度/°CA ATDC-196
转速/(r·min-1600

图1

发动机几何模型"

图2

预燃室几何模型"

表2

边界条件"

边界设置值
进口压力、温度
出口压力、温度
缸盖358 K
活塞347 K
缸套321 K
预燃室顶部400 K
预燃室中部580 K
预燃室底部700 K

图3

网格无关性验证"

图4

模型精度验证"

表3

研究方案"

方案喷射压力/MPa

喷射结束时刻/

℃A ATDC

喷射脉宽/℃A

喷射

量/mg

1-42-160、-120、-80、-50189
5-82-160、-120、-80、-50115.4
9-122-160、-120、-80、-502512.6
13-162-160、-120、-80、-503618
17-201-160、-120、-80、-50256.3
21-241.5-160、-120、-80、-50259.45
25-282.5-160、-120、-80、-502515.75

图5

不同方案下主燃室内压力及瞬时放热率曲线"

图6

不同方案燃烧周期"

图7

不同方案下预燃室内压力及瞬时放热率曲线"

图8

不同方案下温度分布"

图9

高掺氢比、303 K、0.1 MPa下掺氢氨气层流火焰速度随当量比变化"

图10

不同方案点火时刻预燃室内Lambda和燃料掺氢比变化曲线"

图11

不同方案点火时刻预燃室内燃料质量变化曲线"

图12

不同方案点火时刻预燃室内Lambda分布"

图13

不同喷射压力和喷射结束时刻下预燃室内氢气质量变化曲线"

图14

不同喷射压力和喷射结束时刻下喷射结束后预燃室内氢气质量变化曲线"

图15

不同喷射压力和喷射结束时刻下喷射结束后被压回预燃室内氢气质量变化曲线"

图16

不同喷射压力和喷射结束时刻下点火时刻预燃室内氢气质量变化曲线"

图17

不同喷射脉宽和喷射结束时刻下喷射结束后预燃室内氢气质量变化曲线"

图18

不同喷射脉宽和喷射结束时刻下喷射结束后被压回预燃室内氢气质量变化曲线"

图19

不同喷射脉宽和喷射结束时刻下喷射结束后被压回预燃室内氢气质量占其喷氢总量之比的变化曲线"

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