首页> 外文期刊>Journal of Flow Visualization and Image Processing >EXCIPLEX TECHNIQUE FOR SIMULTANEOUS VISUALIZATION OF THE LIQUID AND VAPOR PHASES OF PILOT-INJECTED SPRAY BY LASER-INDUCED FLUORESCENCE
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EXCIPLEX TECHNIQUE FOR SIMULTANEOUS VISUALIZATION OF THE LIQUID AND VAPOR PHASES OF PILOT-INJECTED SPRAY BY LASER-INDUCED FLUORESCENCE

机译:激光诱导荧光同时可视化飞行员喷射喷雾的液相和气相的精确技术

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An optically accessible single-cylinder compression-ignition two-stroke research engine equipped with dual-injection system, image acquisition, and control system have been designed to acquire two-dimensional images of the pilot and main diesel fuel sprays. The engine construction permits illumination of the sprays by a thin sheet of laser light from a pulsed Nd:YAG laser frequency tripled to operate at the ultraviolet wavelength of 355 nm. The liquid fuel was decane with TMPD-naphthalene dopant dispersed in it. After ultraviolet excitation by the pulsed laser, liquid fuel regions fluoresced with a spectrum centered at the wavelength of 380 nm, while vapor regions fluoresced with a spectrum centered at 470 nm. This approach, called Exciplex technique, was applied to permit simultaneous acquisition of the liquid and vapor fuel regions in the cup-in-head geometry of the combustion chamber. The results from limited conditions suggest that existence of the pilot injection affects the chamber flow field, particularly in the near-wall region, in such a way that less liquid fuel accumulation occurs with pilot injection scheme thus should reduce hydrocarbon emission. The area spreading rate of both vapor and liquid phases within the visualization plane were linear in early stages with former having a higher rate. Close to the impingement time, vapor phase area penetration is reduced to near zero, while liquid continues linearly but at slower rate than its initial value. Both air utilization and evaporization are therefore reduced. Also, based on this and -work by others, the suggestion is made that to achieve optimum simultaneous reduction in soot and NO_x, the timing between the pilot and main injections (dwell) should be chosen with due consideration of the interaction between the swirl flow and pilot spray and the relative magnitudes of the ignition delay period with respect to the dwell.
机译:配备双喷射系统,图像采集和控制系统的可光学访问的单缸压燃式二冲程研究型发动机已经过设计,可采集飞行员和主要柴油喷雾的二维图像。发动机结构允许来自脉冲Nd:YAG激光频率的三倍薄的激光照亮喷雾,并在355 nm的紫外线波长下工作。液体燃料是癸烷,其中分散有TMPD-萘掺杂剂。在脉冲激光的紫外激发之后,液体燃料区域发荧光的光谱以380 nm为中心,而蒸汽区域发荧光的光谱以470 nm为中心。这种方法称为Exciplex技术,用于允许同时获取燃烧室杯形杯头几何形状中的液体和蒸气燃料区域。有限条件下的结果表明,先导喷射的存在会影响腔室流场,尤其是在近壁区域,从而使先导喷射方案中发生的液体燃料积聚更少,因此应减少碳氢化合物的排放。可视化平面内汽相和液相的面积扩散率在早期阶段都是线性的,前者的扩散率更高。接近撞击时间,气相面积渗透率降低到接近零,而液体以线性方式继续,但速率比其初始值慢。因此,减少了空气利用和蒸发。另外,基于此以及其他人的工作,建议为实现烟灰和NO_x的最佳同时减少,应适当考虑旋流之间的相互作用来选择引燃和主喷射(停留)之间的时间点火喷雾和点火延迟时间相对于停留时间的相对大小。

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    Engine Eaboratory, Department of Mechanical Engineering (MIC 251), University of Illinois at Chicago, 842 West Taylor Street, Chicago, Illinois 60607-7022;

    Engine Eaboratory, Department of Mechanical Engineering (MIC 251), University of Illinois at Chicago, 842 West Taylor Street, Chicago, Illinois 60607-7022;

    GMI (General Motors Institute) Engine Eaboratory, GMI Engineering and Management Institute, Department of Mechanical Engineering, 1700 W. Third Ave, Flint, MI 48504-4898;

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