Cooling enhancement for engine parts using jet impingement

IF 2 Q2 ENGINEERING, MECHANICAL Frontiers in Mechanical Engineering Pub Date : 2024-01-18 DOI:10.3389/fmech.2024.1251587
G. Nasif, A.-M. Shinneeb, R. Balachandar
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Abstract

A computational study has been performed to evaluate the use of jet impingement for cooling applications in the automotive industry. The current study uses an entire internal combustion engine cylinder with its components as a computational domain. An unsteady numerical solution for the Navier-Stokes equations was carried out using Improved Delayed Detached Eddy Simulation (IDDES). The volume of fluid approach is proposed to track and locate the liquid jet surface that is in contact with the air. The conjugate heat transfer approach is used to link the heat transfer solution between the fluid and the solid. The boundary conditions that are employed in the study are provided from lab experiments and one-dimensional simulations. The cooling jet in this study targets the hottest region in the piston, i.e., the region underneath the exhaust valve. Three nozzle sizes with flows at different Reynolds numbers are chosen to examine the thermal characteristics of the cooling jet. The computational study reveals that for a specific Reynolds number, the smaller diameter nozzle provides the highest heat transfer coefficient around the impingement point. The maximum relative velocity location at the impingement point slightly leads the location of the maximum Nusselt number. The maximum temperature in the piston decreases by 7% to 11% as the nozzle diameter changes from 1.0 to 3.0 mm for a jet Reynolds number of 4,500. If a correct selection is made for the nozzle size, the cooling jet can be efficiently used to reduce the temperature and alleviate the thermal stresses in the piston in the region underneath the exhaust valve where the maximum temperature occurs.
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利用射流冲击增强发动机部件的冷却效果
我们进行了一项计算研究,以评估喷射撞击在汽车工业冷却应用中的应用。当前的研究使用整个内燃机气缸及其部件作为计算域。使用改进的延迟分离涡模拟(IDDES)对纳维-斯托克斯方程进行了非稳态数值求解。提出了流体体积法来跟踪和定位与空气接触的液体喷射面。共轭传热方法用于连接流体和固体之间的传热解决方案。研究中采用的边界条件来自实验室实验和一维模拟。本研究中的冷却射流针对活塞中最热的区域,即排气阀下方的区域。为了研究冷却射流的热特性,我们选择了三种尺寸的喷嘴和不同雷诺数的流量。计算研究表明,对于特定的雷诺数,直径较小的喷嘴在撞击点周围的传热系数最高。撞击点的最大相对速度位置略微领先于最大努塞尔特数的位置。在射流雷诺数为 4,500 时,喷嘴直径从 1.0 毫米变为 3.0 毫米时,活塞内的最高温度降低了 7% 至 11%。如果正确选择喷嘴尺寸,就可以有效利用冷却射流来降低温度,并减轻排气阀下方出现最高温度区域的活塞热应力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Frontiers in Mechanical Engineering
Frontiers in Mechanical Engineering Engineering-Industrial and Manufacturing Engineering
CiteScore
4.40
自引率
0.00%
发文量
115
审稿时长
14 weeks
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