首页> 外文会议>9th Annual Conference on Liquid Atomization and Spray Systems(ILASS-ASIA 2004) >A study on the spray structure and evaporation characteristic of common rail type high pressure injector in homogeneous charge compression ignition engine
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A study on the spray structure and evaporation characteristic of common rail type high pressure injector in homogeneous charge compression ignition engine

机译:均质充量压燃式发动机共轨式高压喷油器的喷雾结构和蒸发特性研究

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The purpose of this study was to investigate the spray structure and evaporation characteristics of common rail high pressure injector for use in a direct injection type HCCI (Homogeneous Charge Compression Ignition) engine. In this study, we measured the injection rate and visualized the spray structure of a HCCI injector according to injection conditions. The CFD simulation of the spray and the air fuel mixture formation in real engine conditions was also conducted using the VECTIS commercial code. In addition, we compared simulation results to experimental results. From the spray experiment and simulation results, we found the spray penetration to be proportional to back pressure by an exponent of 1/4. This is similar to Hiroyasu's experimental result. The fuel evaporation and air fuel mixture result indicate that the influence of the spray impingement with the ambient density was bigger than that of the intake pressure and temperature conditions in evaporation rate when the fuel was injected at the early stage of the compression stroke. The results also reveal that the fuel was uniformly distributed in the combustion chamber at this early injection time and that the air fuel mixture enhanced in this relatively rich region. However, when ambient density was kept constant, the fuel evaporation was sensitive to the influence of the intake temperature and pressure. As the fuel was injected at the later stage of the compression stroke the fuel tended to concentrate in the bowl zone and the air fuel mixture enhanced in the lean region. From these results it was confirmed that the air fuel mixture characteristics are sensitive to the impingement position of the injected fuel.
机译:这项研究的目的是研究用于直接喷射式HCCI(均质充量压缩点火)发动机的共轨高压喷射器的喷雾结构和蒸发特性。在这项研究中,我们测量了注射速率,并根据注射条件可视化了HCCI注射器的喷雾结构。还使用VECTIS商业代码对实际发动机条件下的喷雾和空气燃料混合物形成进行了CFD模拟。此外,我们将仿真结果与实验结果进行了比较。从喷雾实验和模拟结果中,我们发现喷雾渗透与反压成比例,为1/4。这与弘安的实验结果相似。燃料蒸发和空气燃料混合的结果表明,当在压缩冲程的早期喷射燃料时,喷雾撞击对环境密度的影响大于进气压力和温度条件对蒸发速率的影响。结果还表明,在该较早的喷射时间,燃料均匀地分布在燃烧室中,并且空气燃料混合物在该相对富集的区域中增强。但是,当环境密度保持恒定时,燃油蒸发对进气温度和压力的影响很敏感。当在压缩冲程的后期喷射燃料时,燃料趋向于集中在碗形区域中,并且空气燃料混合物在稀区域中增强。从这些结果证实,空气燃料混合物特性对喷射燃料的撞击位置敏感。

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