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Optimizing Cooling Fan Power Consumption for Improving Diesel Engine Fuel Efficiency Using CFD Technique

机译:优化冷却风扇功耗,采用CFD技术改善柴油发动机燃料效率

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Fan cooling system of an air-cooled diesel engine is optimized using 3D CFD numerical simulation approach. The main objective of this article is to increase engine fuel efficiency by reducing fan power consumption. It is achieved by optimizing airflow rates and flow distribution over the engine surfaces to keep the maximum temperature of engine oil and engine surfaces well within the lubrication and material limit, respectively, at the expense of lower fan power. Based on basic fan laws, a bigger fan consumes lesser power for the same airflow rate as compared to a smaller fan, provided both fans have similar efficiency. Flow analysis is also conducted with the engine head and block modeled as solid medium and fan cooling system as fluid domain. Reynolds-averaged Navier-Stokes turbulence (RANS) equations were solved to get the flow field inside the cooling system and on the engine liner fins. The Moving Reference Frame approach was used for simulating the rotation of a fan. Cowl geometry was modified for providing better guidance to flow over engine surfaces and to get maximum utilization of cooling capacity of flowing air. Basic fan parameters like diameter, blade shape, and number of blades were altered to increase the flow rate and reduce fan power consumption. Engine surface temperature is compared between existing and recommended design modified on actual engine test bed. The final recommended design leads to a 3% improvement in engine fuel efficiency, i.e., engine fan power consumption reduction. It is achieved with comparable engine surface temperature.
机译:使用3D CFD数值模拟方法优化风扇冷却系统,使用3D CFD数值模拟方法进行了优化。本文的主要目标是通过减少风扇功耗来提高发动机燃料效率。通过优化发动机表面上的气流速率和流量分布来实现发动机油和发动机表面的最高温度,分别以较低的风扇功率牺牲润滑和材料限制的最大温度。基于基本粉丝定律,与较小的风扇相比,更大的风扇为与较小风扇相比,相同的气流速率消耗较小的电源,只要两个风扇都具有相似的效率。流动分析也用发动机头部和块作为固体介质和风扇冷却系统为流体域进行进行。 Reynolds-Iveriged Navier-Stokes湍流(RANS)方程被解决以使冷却系统内部和发动机衬垫翅片内的流场。移动参考帧方法用于模拟风扇的旋转。修改了牛仔几何形状,以提供更好的引导来流过发动机表面并获得最大限度地利用流动空气的冷却能力。改变了基本风扇参数,如直径,刀片形状和叶片数量,以增加流量并降低风扇功耗。在实际发动机试验台上修改的现有和推荐设计之间比较发动机表面温度。最终推荐的设计导致发动机燃料效率的提高3%,即发动机风扇功耗降低。它是通过相当的发动机表面温度实现的。

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