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基于激光诊断技术的汽油直喷发动机喷雾机理

尚勇 金伟

尚勇, 金伟. 基于激光诊断技术的汽油直喷发动机喷雾机理[J]. 北京航空航天大学学报, 2020, 46(1): 60-66. doi: 10.13700/j.bh.1001-5965.2019.0178
引用本文: 尚勇, 金伟. 基于激光诊断技术的汽油直喷发动机喷雾机理[J]. 北京航空航天大学学报, 2020, 46(1): 60-66. doi: 10.13700/j.bh.1001-5965.2019.0178
SHANG Yong, JIN Wei. Mechanism of spray in gasoline direct injection engine based on laser diagnostics[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(1): 60-66. doi: 10.13700/j.bh.1001-5965.2019.0178(in Chinese)
Citation: SHANG Yong, JIN Wei. Mechanism of spray in gasoline direct injection engine based on laser diagnostics[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(1): 60-66. doi: 10.13700/j.bh.1001-5965.2019.0178(in Chinese)

基于激光诊断技术的汽油直喷发动机喷雾机理

doi: 10.13700/j.bh.1001-5965.2019.0178
详细信息
    作者简介:

    尚勇  男, 博士, 副研究员。主要研究方向:内燃机喷雾及燃烧基础理论、装备制造业发展及政策

    金伟  男, 硕士, 副研究员。主要研究方向:装备制造技术发展及政策

    通讯作者:

    金伟,E-mail:18801136122@126.com

  • 中图分类号: TK401

Mechanism of spray in gasoline direct injection engine based on laser diagnostics

More Information
  • 摘要:

    汽油直喷喷雾贯穿度、锥角等宏观喷雾特性,对研究汽油直喷发动机喷雾及燃烧的发生、发展具有重要意义。在设计并建立汽油直喷(GDI)系统的基础上,搭建定容燃烧弹系统和激光测试系统,基于LSD测试技术,研究了喷油压力和背景压力对汽油直喷宏观喷雾特性的影响。通过试验发现,随喷油压力增加,相同喷油时刻下的贯穿度逐渐增加。随背景压力增加,相同喷油时刻下的贯穿度逐渐减少。在不同喷油压力和背景压力下,随着喷射时间的发展,贯穿度均逐渐增加,喷雾锥角为38°~50°。

     

  • 图 1  Nd:YAG激光器

    Figure 1.  Nd:YAG laser

    图 2  图像采集系统

    Figure 2.  Image acquisition system

    图 3  定容喷雾试验专用容弹

    Figure 3.  Constant volume combustion bomb for spray test

    图 4  汽油直喷系统

    Figure 4.  Gasoline direct injection system

    图 5  试验系统

    Figure 5.  Experimental system

    图 6  LIF拍摄图片(变喷油压力)

    Figure 6.  LIF picture (variable injection pressure)

    图 7  Mie拍摄图片(变喷油压力)

    Figure 7.  Mie picture (variable injection pressure)

    图 8  喷雾贯穿度随喷油压力的变化规律

    Figure 8.  Variation rule of spray penetration with injection pressure

    图 9  喷雾锥角随喷油压力的变化规律

    Figure 9.  Variation rule of spray cone angle with injection pressure

    图 10  LIF拍摄图片(变背景压力)

    Figure 10.  LIF picture (variable back pressure)

    图 11  喷雾贯穿度随背景压力的变化规律

    Figure 11.  Variation rule of spray penetration with back pressure

    图 12  喷雾锥角随背景压力的变化规律

    Figure 12.  Variation rule of spray cone angle with back pressure

    表  1  试验方案

    Table  1.   Test scheme

    试验工况 喷油压力/MPa 背景压力/MPa
    变喷油压力 1、3、5、7、9 0.1
    变背景压力 5 0.1、0.5、1、1.5
    下载: 导出CSV
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出版历程
  • 收稿日期:  2019-04-22
  • 录用日期:  2019-05-10
  • 网络出版日期:  2020-01-20

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