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Investigation of Spray and Combustion of a Piezoelectric Fuel Injector for Gasoline Direct Injection Engines

机译:汽油直喷发动机的压电燃料喷射器的喷雾和燃烧研究

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摘要

In recent years, more stringent emission standard and high fuel economy demands have forced vehicle manufactures to seek alternative techniques to synchronize benefits of both gasoline and diesel fuels. In this work, experimental studies of spray characteristics and fuel auto-ignition properties from an outwardly opening piezoelectric gasoline direct injection fuel injector were conducted in an optically accessible constant volume combustion chamber (CVCC) experiment system.;Fuel sprays of light naphtha (LN), primary reference fuel (PRF), and E10 gasoline under different ambient pressures from 1 bar to 12.5 bar were investigated first. Spray was visualized by applying a Mie-scattering technique. A high-speed camera was employed to capture the spray images. Results show that a clear filamentary hollow-cone spray structure is formed for all three fuels at atmospheric conditions, and toroidal recirculation vortices are observed at the downstream spray edges. A higher ambient pressure leads to a stronger vortex located closer to the injector outlet. Larger spray angles are found under higher ambient pressure conditions for all three fuels.;Ambient pressure conditions were then extended to a lower range for iso-octane sprays. Five ambient pressure conditions were selected from 0.01 bar to 0.10 bar to evaluate the effect of superheated conditions on the spray structure from the piezoelectric fuel injector. Results indicate that spray under a superheated condition presents a distinct spray structure in the flash boiling regime. A lower ambient pressure within the superheated condition range results in a stronger deformation on spray structure, a faster spray front penetration velocity and a faster liquid vaporization rate. These phenomena are dominated by ambient pressures. Effects of fuel the injection pressure and the fuel injection duration are relatively negligible.;Next, the auto-ignition characteristics of LN, primary reference fuels (PRF65, PRF95), gasoline (Haltermann CARB LEV III) and a gasoline surrogate under conditions similar to the spray G condition (3.5 kg/m3 gas density, 21% ambient oxygen concentration) were studied. Five different ambient temperatures from 650 K to 950 K with a 75 K step were investigated. Fuel auto-ignition was observed with noticeable ignition delay for five investigated fuels under all selected experiment conditions. Results show that the locations of the occurrence of autoignitions are randomly distributed in combustion chamber. Ignition delay of each fuel is always longer than fuel injection duration under all selected experiment conditions. Differences in ignition delay among the five fuels are more significant when the ambient temperature is lower than 750K.;At last, two-color measurements were conducted for LN under diesel engine conditions. Five ambient oxygen concentrations varying from 10% to 21% and three ambient temperature conditions, 800K, 100K and 1200K, were selected to simulate both conventional diesel engine operation environment and low temperature and low oxygen concentration environment. Flame temperature distribution and KL factor distribution under different ambient conditions were calculated and discussed.
机译:近年来,更严格的排放标准和更高的燃油经济性要求迫使汽车制造商寻求替代技术来同步汽油和柴油燃料的利益。在这项工作中,在光学可访问的恒容燃烧室(CVCC)实验系统中进行了向外打开的压电汽油直喷燃料喷射器对喷雾特性和燃料自燃特性的实验研究。首先研究了在从1 bar到12.5 bar的不同环境压力下的,初级参考燃料(PRF)和E10汽油。通过应用米氏散射技术使喷雾可视化。使用高速相机捕获喷雾图像。结果表明,在大气条件下,所有三种燃料均形成了清晰的丝状空心锥喷雾结构,并且在下游喷雾边缘观察到了环形再循环涡流。较高的环境压力会导致更强的涡流位于更靠近喷油器出口的位置。在所有三种燃料的较高环境压力条件下均发现较大的喷雾角度。然后,将异辛烷喷雾的环境压力条件扩展至较低范围。从0.01 bar到0.10 bar中选择了五个环境压力条件,以评估过热条件对压电燃料喷射器的喷雾结构的影响。结果表明,过热条件下的喷雾在闪蒸状态下呈现出独特的喷雾结构。在过热条件范围内较低的环境压力会导致喷雾结构变形更强,喷雾前沿渗透速度更快,液体汽化速率也更快。这些现象主要受环境压力的影响。燃油喷射压力和燃油喷射持续时间的影响相对可以忽略不计;其次,LN,主要参考燃料(PRF65,PRF95),汽油(Haltermann CARB LEV III)和汽油替代物在类似条件下的自燃特性研究了喷雾G条件(气体密度为3.5 kg / m3,环境氧气浓度为21%)。研究了从650 K到950 K的5个不同的环境温度,步长为75K。在所有选定的实验条件下,观察到的五种被调查燃料的燃料自动点火均具有明显的点火延迟。结果表明,自燃发生的位置在燃烧室内是随机分布的。在所有选定的实验条件下,每种燃料的点火延迟始终长于燃料喷射持续时间。当环境温度低于750K时,五种燃料的点火延迟差异更大。最后,在柴油机条件下对LN进行了两种颜色的测量。选择了5种环境氧浓度(从10%到21%不等)和3种环境温度条件(800K,100K和1200K)来模拟常规柴油机运行环境和低温低氧浓度环境。计算并讨论了不同环境条件下的火焰温度分布和KL因子分布。

著录项

  • 作者

    Wu, Zengyang.;

  • 作者单位

    North Carolina State University.;

  • 授予单位 North Carolina State University.;
  • 学科 Mechanical engineering.
  • 学位 Ph.D.
  • 年度 2017
  • 页码 175 p.
  • 总页数 175
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:36:46

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