首页> 外文会议>SAE Brasil Congress Exhibition >Finned surfaces in air-cooled internal combustion engine: influence of geometry and flow conditions
【24h】

Finned surfaces in air-cooled internal combustion engine: influence of geometry and flow conditions

机译:空冷内燃机中的翅片表面:几何和流动条件的影响

获取原文

摘要

The internal combustion engine cooling is very important to its proper functioning, since high temperatures can shorten the durability of internal components and hence increase fuel consumption. In air-cooled engines it is common to use extended surfaces (fins), which provide an increase in the convective and radiative heat exchange. Thus, the present work investigates the phenomenon of convection between the external air and the motor casing through computational simulations. The finite differences method was applied for two fin geometry (annular and rectangular). The temperature distribution and the heat transfer rate in the fin were obtained for different ambient temperatures (20 - 40 °C) and flow rates (0 - 25 m/s). The analysis was based on a typical 150-cylinder motorcycle engine with fins made of 204-aluminum alloy. It was observed that under zero flow conditions and ambient temperature of 30 °C there was a temperature gradient of 38.49 °C on the annular fins and only 7.76 °C on the rectangular ones. For forced convection conditions (at 25 m / s) the gradient on the annular fins was 71.60 °C and on the rectangular ones 41.23 °C. If the ambient temperature is increased by 10 °C there is a decrease in the temperature gradient in the fins. However, decreasing the ambient temperature by 10 °C, the gradient undergoes little variation. Furthermore, although they have higher thermal gradients, the annular fins have had lower thermal exchange values (up to 40% less), because the area in such geometry is somewhat smaller than for the rectangular geometry. Therefore, the present work contributes to the area by providing thermal data to verify the appropriate cooling means, fin geometry and conditions, as well as providing the basis for the indication of the best fin system model to be used.
机译:内燃机冷却对其正常运行非常重要,因为高温可以缩短内部部件的耐久性,从而提高燃料消耗。在风冷的发动机中,通常使用扩展表面(翅片),这提供了对流和辐射热交换的增加。因此,本作通过计算模拟研究了外部空气和电动机壳体之间的对流现象。施加有限差异方法两种翅片几何(环形和矩形)。为不同的环境温度(20-40℃)和流速(0-25m / s)获得翅片中的温度分布和传热速率。该分析基于典型的150缸摩托车发动机,其具有由204-铝合金制成的翅片。观察到,在零流动条件下,在30℃的环境温度下,在环形翅片上存在38.49℃的温度梯度,并且在矩形中仅为7.76℃。对于强制对流条件(25米/秒),环形翅片上的梯度为71.60°C,在矩形41.23°C上。如果环境温度增加10°C,则翅片中的温度梯度降低。然而,将环境温度降低10°C,梯度经历几乎没有变化。此外,虽然它们具有更高的热梯度,但是环形翅片具有较低的热交换值(高达40%),因为这种几何形状中的区域比矩形几何形状小。因此,通过提供热数据来验证适当的冷却装置,鳍几何和条件以及为要使用的最佳鳍系统模型的指示提供基础,为该区域提供给该地区。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号