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Improving Cylinder Cooling Using Tapered Fins and Baffle Plates Between Fins in Air-Cooled Engines

机译:在风冷发动机翅片之间使用锥形翅片和挡板改善汽缸冷却

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We aim to maximize the performance of air-cooled engines (such as motorbike engines and small stationary engines) by increasing cylinder cooling and by maintaining uniform temperature around the cylinder circumference. In typical engine designs, air cools the front of the cylinder better than the rear. In an effort to increase cooling at the rear, this research experiments with tapered fins that contract air flow to the cylinder axis between the fins, and with baffle plates mounted between fins symmetrically with respect to a plane through the axis of the cylinder. In a wind tunnel at air velocities between 20 and 60 km/h, we compared cylinders with conventional fins, cylinders with tapered fins, cylinders with baffle plates between conventional fins, and cylinders with baffle plates between tapered fins. We measured the temperature inside the cylinder to determine the heat release, and we measured the temperature on the fin surface to determine the temperature distribution around the cylinder circumference. We also visualized the air flow over the fin surface, using the oil film method, and between fins, using the smoke wire method, to understand how tapered fins and baffle plates contributed to cylinder cooling. Results indicate that both tapered fins and conventional fins with baffle plates between fins increased cylinder cooling, compared with conventional fins without baffle plates. Furthermore, our cylinder fitted with both tapered fins with the tapered portion closest to the rear, and baffle plates between fins, enjoyed the greatest cylinder cooling.
机译:我们的目的是通过增加汽缸冷却并通过保持圆柱圆周的均匀温度来最大限度地提高空气冷却发动机(例如摩托车发动机和小固定式发动机)的性能。在典型的发动机设计中,空气比后部更好地冷却圆筒的前部。努力在后部增加冷却,这项研究实验与锥形翅片一起收缩到翅片之间的气缸轴线的锥形翅片,并且挡板平板相对于穿过汽缸的轴线对称地对称地。在20至60 km / h之间的风速下的风洞中,我们将气缸与传统的翅片,带锥形翅片的圆柱体进行比较,具有传统翅片之间的挡板和带挡板之间的挡板之间的挡板的圆柱体。我们测量气缸内的温度以确定热释放,并测量翅片表面上的温度以确定圆柱圆周周围的温度分布。我们还使用烟丝法在翅片表面上的空气流动,使用烟丝方法,以了解锥形翅片和挡板如何导致气缸冷却。结果表明,与没有挡板的常规鳍片相比,锥形翅片和翅片在翅片之间的挡板与挡板之间的传统翅片增加了圆柱形冷却。此外,我们的圆柱装配有两个锥形翅片,锥形部分最靠近后部,翅片之间的挡板,圆柱形冷却最大。

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