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Flow losses at circular T-junctions representative of intake plenum and primary runner interface

机译:进气压力通风界和主要跑步者界面的圆形T型交叉点的流量损失

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One of the dominant sources of flow losses in the intake system of internal combustion engines (ICE) with log-style manifolds is the interface between the plenum and primary runner. The present study investigates such losses associated with the dividing flow at the entry to primary runner with geometries representative of those used in ICE. An experimental setup was constructed to measure the flow loss coefficients of T-junctions with all branches of circular cross-section. Experiments were conducted with seven configurations on a steady-flow bench to determine the effects of: (1) interface radius equal to 0, 10, and 20% of the primary runner diameter, (2) plenum to primary runner area ratios of 1, 2.124, and 3.117, and (3) primary runner taper including taper area ratios of 2.124 and 3.117. The last two categories employed 20% interface radii. The total mass flow rate was also varied to investigate the effect of Reynolds number Re on loss coefficients. Interface radii and primary runner taper were found to significantly reduce the losses. In the turbulent regime, loss coefficients were found to be reasonably independent of Reynolds number. A subset of results presented here was compared with the available literature.
机译:带有符号风格歧管的内燃机(ICE)进气系统中的主要流量损失源之一是增压室和主要转轮之间的界面。本研究调查了与初级跑步者的分裂流相关的这种损失,几何形状代表冰中使用的物质。构建实验装置以测量与圆形横截面的所有分支的T型交配的流量损失系数。在稳态台上进行七种配置进行实验,以确定:(1)界面半径等于0,10,20%的主要转子直径,(2)到主要转轮面积比为1, 2.124和3.117,(3)主要跑步锥度,包括2.124和3.117的锥形面积比。最后两类采用20%接口半径。还可以改变总质量流量,以研究Reynolds数Re在损耗系数上的效果。接口半径和主要跑步锥度被发现显着降低了损失。在湍流状态下,发现损失系数合理地独立于雷诺数。将在此呈现的结果与可用文献进行比较。

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