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Characterisation of Spray Development from Spark-Eroded and Laser-Drilled Multihole Injectors in an Optical DISI Engine and in a Quiescent Injection Chamber

机译:光学DIsI发动机和静态注入室中火花侵蚀和激光钻孔多孔注射器喷雾发展的表征

摘要

This paper addresses the need for fundamental understanding of the mechanisms of fuel spray formation and mixture preparation in direct injection spark ignition (DISI) engines. Fuel injection systems for DISI engines undergo rapid developments in their design and performance, therefore, their spray breakup mechanisms in the physical conditions encountered in DISI engines over a range of operating conditions and injection strategies require continuous attention. In this context, there are sparse data in the literature on spray formation differences between conventionally drilled injectors by spark erosion and latest Laser-drilled injector nozzles. A comparison was first carried out between the holes of spark-eroded and Laser-drilled injectors of same nominal type by analysing their in-nozzle geometry and surface roughness under an electron microscope. Then the differences in their spray characteristics under quiescent conditions, as well as in a motoring optical engine, are discussed on the basis of high-speed imaging experiments and image processing methods. Specifically, the spray development mechanism was quantified by spray tip penetration and cone angle data under a range of representative low-load and high-low engine operating conditions (0.5 bar and 1.0 bar absolute, respectively), as well as at low and high injector body temperatures (20 °C and 90 °C) to represent cold and warm engine-head conditions. Droplet sizing was also performed with the two injectors using Phase Doppler Anemometry in a quiescent chamber.
机译:本文提出了对直喷式火花点火(DISI)发动机中燃料喷雾形成和混合物制备机理的基本理解的需求。用于DISI发动机的燃油喷射系统的设计和性能正在快速发展,因此,在一系列操作条件和喷射策略下,DISI发动机在物理条件下遇到的喷雾破裂机制需要不断关注。在这种情况下,文献中很少有关于通过火花腐蚀和传统的激光钻孔喷嘴之间的传统钻孔喷嘴之间的喷雾形成差异的数据。首先通过在电子显微镜下分析它们的喷嘴内几何形状和表面粗糙度,对具有相同标称类型的火花腐蚀和激光钻孔的喷射器的孔之间进行比较。然后,在高速成像实验和图像处理方法的基础上,讨论了在静态条件下以及在驱动光学引擎中其喷雾特性的差异。具体而言,在一系列典型的低负荷和高低发动机工况(分别为0.5 bar和1.0 bar绝对压力)以及低喷射器和高喷射器的条件下,通过喷嘴尖端渗透和锥角数据对喷雾形成机理进行了量化。机体温度(20°C和90°C)代表冷和热的发动机盖状况。还使用两个注射器在静态室内使用相多普勒风速仪对液滴进行了尺寸测定。

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