首页> 外文期刊>Journal of Energy Resources Technology >The Effect of the Helical Inlet Port Design and the Shrouded Inlet Valve Condition on Swirl Generation in Diesel Engine
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The Effect of the Helical Inlet Port Design and the Shrouded Inlet Valve Condition on Swirl Generation in Diesel Engine

机译:螺旋进气道设计和带盖进气门状况对柴油机涡流产生的影响

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摘要

Inlet port design has a great influence on swirl generation inside the engine cylinder. In this paper, two helical inlet ports having the same helix design were suggested. The first has an upper entrance, and the second has a side entrance. With the two ports, shrouded inlet valves having different conditions of shroud and orientation angles were used. Four shroud angles were used; they are 90 deg, 120 deg, 150 deg, and 180 deg. Also, four orientation angles were used; they are 0 deg, 30 deg, 60 deg, and 90 deg. Three-dimensional simulation model using the shear stress transport k– ω model was used for predicting the air flow characteristics through the inlet port and the engine cylinder in both intake and compression strokes. The results showed that the side entrance port produces swirl ratio higher than that of the upper entrance port by about 3.5%, while the volumetric efficiency is approximately the same for both ports. For both the ports, increasing the valve shroud angle increases the swirl ratio and reduces the volumetric efficiency. The maximum increments of swirl ratio relative to the ordinary valve case occur at valve conditions of 30–150 deg, 0–180 deg, and 30–180 deg. At these valve conditions, the swirl ratio values are 6.38, 6.72, and 6.95 at intake valve close (IVC) with percentage increments of 69.2%, 78.2%, and 84.4%, respectively. The corresponding values of the volumetric efficiency are 93.6, 92.5, and 91.2, respectively, with percentage decrements of 2.84%, 4%, and 5.7%, respectively.
机译:进气口设计对发动机气缸内的涡流产生有很大影响。在本文中,建议使用两个螺旋设计相同的螺旋形进气口。第一个有一个上部入口,第二个有一个侧面入口。对于这两个端口,使用了具有不同护罩和定向角度条件的有护罩的进气阀。使用了四个护罩角;它们分别是90°,120°,150°和180°。另外,使用了四个取向角。它们是0°,30°,60°和90°。使用剪切应力传输k– ω模型的三维模拟模型来预测进气和压缩冲程中通过进气道和发动机气缸的气流特性。结果表明,侧进气道产生的涡流比高出进气道的涡流比高约3.5%,而两个进气道的容积效率大致相同。对于两个端口,增加阀罩角度都会增加涡流比并降低容积效率。相对于普通阀壳,最大涡旋比增量出现在30–150°deg,0-180°deg和30-180°deg的气门状态下。在这些气门条件下,进气门关闭(IVC)时的涡流比值为6.38、6.72和6.95,百分比增量分别为69.2%,78.2%和84.4%。容积效率的相应值分别为93.6、92.5和91.2,百分比减小分别为2.84%,4%和5.7%。

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