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发动机活塞冷却喷嘴射流特性数值模拟与试验研究
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Numerical simulation and experimental study on jet flow characteristics of engine piston cooling nozzle
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    摘要:

    针对高强化发动机活塞冷却系统的优化需求, 建立基于分散流体体积法(dispersed volume of fluid, dispersed-VOF)的活塞冷却喷嘴射流CFD模型, 引入气相体积分数, 结合高速摄像试验结果对模型进行多工况校验, 研究了活塞冷却喷嘴的射流特性及其影响机制. 基于射流速度、湍流强度与耗散、发散角等参数, 分析了发动机转速(600~1 800 r/min)和冷却喷嘴长径比(1~6)对射流特性的影响规律. 研究首次量化揭示了射流气相体积分数、发散角与发动机转速的线性关系:转速每增加300 r/min, 气相体积分数平均下降4.2%、射流发散角平均增大0.14°;发现长径比为4的喷嘴在工作过程中具有相对优异的射流发散特性与湍流强度, 能够有效提升进油效率并增强冷却效果.

    Abstract:

    To meet the optimization demands of the piston cooling system in a highly enhanced engine, a CFD model of the piston cooling nozzle jet based on the Dispersed-VOF method was established. The model incorporated the gas volume fraction and was validated by the results of the high-speed camera test under multiple operating conditions. The jet characteristics of the piston cooling nozzle and their influencing mechanisms were systematically investigated. Based on the parameters of jet velocity, turbulence intensity and dissipation, and divergence angle, the influences of engine speed (600~1 800 r/min) and length-diameter ratio of cooling nozzle (1~6) on jet characteristics were analyzed. This study provides the first quantitative revelation of the linear relationship between the gas volume fraction of the jet and engine speed, as well as the linear relationship between the divergence angle and engine speed: for every increase of 300 r/min in engine speed, the gas volume fraction is decreased by an average of 4.2%, and the jet divergence angle is increased by an average of 0.14°. It also finds that the nozzle with a length - diameter ratio of 4 exhibits relatively superior jet divergence characteristics and turbulence intensity during operation, which can effectively improve the oil intake efficiency and enhance the cooling effect.

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周长江 ?,唐珊 ,刘亚辉 ,马寅杰 .发动机活塞冷却喷嘴射流特性数值模拟与试验研究[J].湖南大学学报:自然科学版,2026,53(4):62~70

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  • 在线发布日期: 2026-05-06
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