Characterization of Flow Asymmetry During the Compression Stroke Using Swirl-Plane PIV in a Light-Duty Optical Diesel Engine with the Re-entrant Piston Bowl Geometry

活塞(光学) 不对称 表征(材料科学) 材料科学 平面(几何) 流量(数学) 圆柱 机械 压缩(物理) 四冲程发动机 冲程(发动机) 光学 几何学 机械工程 物理 工程类 复合材料 数学 纳米技术 燃烧室 燃烧 波前 有机化学 化学 量子力学
作者
Kan Zha,Stephen Busch,Paul C. Miles,Sameera Wijeyakulasuriya,Saurav Mitra,P. K. Senecal
出处
期刊:SAE International journal of engines [SAE International]
卷期号:08 (4): 1837-1855 被引量:47
标识
DOI:10.4271/2015-01-1699
摘要

<div class="section abstract"><div class="htmlview paragraph">Flow field asymmetry can lead to an asymmetric mixture preparation in Diesel engines. To understand the evolution of this asymmetry, it is necessary to characterize the in-cylinder flow over the full compression stroke. Moreover, since bowl-in-piston cylinder geometries can substantially impact the in-cylinder flow, characterization of these flows requires the use of geometrically correct pistons. In this work, the flow has been visualized via a transparent piston top with a realistic bowl geometry, which causes severe experimental difficulties due to the spatial and temporal variation of the optical distortion. An advanced optical distortion correction method is described to allow reliable particle image velocimetry (PIV) measurements through the full compression stroke.</div><div class="htmlview paragraph">Based on the ensemble-averaged velocity results, flow asymmetry characterized by the swirl center offset and the associated tilting of the vortex axis is quantified. The observed vertical tilting of swirl center axis is similar for tested swirl ratios (2.2 and 3.5), indicating that the details of the intake flows are not of primary importance to the late-compression mean flow asymmetry. Instead, the geometry of the piston pip likely impacts the flow asymmetry.</div><div class="htmlview paragraph">The PIV results also confirm the numerically simulated flow asymmetry in the early and late compression stroke: at BDC, the swirl center is located closer to the exhaust valves for swirl-planes farther away from the fire deck; near TDC, the swirl center is located closer to the intake valves for swirl-planes farther away from the fire deck. It is evident from experimentally determined velocity fields that the transition between these two asymmetries has a different path for various swirl ratios, suggesting the influence of intake port flows.</div></div>
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