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KIVA程序是一功能比较齐全的内燃机缸内过程模拟数值计算的大型程序,它代表了目前多维模型的最新进展。本文论述了KIVA程序中喷雾模型的发展历程和进展,最后指出了燃油喷雾多维模型研究的发展趋向。 相似文献
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搭载柴油机的小型、紧凑型车辆中,每缸两气门设计的柴油机仍然占有相当大的市场份额。论述了对1台1.2 L 每缸两气门柴油机中气道-气门-缸内气流的数值模拟研究,以描述其进气歧管和进气道的性能。 相似文献
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本文中应用大涡模拟方法对一台四气门单缸光学发动机进行了100个连续周期冷态流场计算,计算结果通过了PIV实验验证,为缸内湍流场拟序结构的研究构建了可靠的数据库。然后应用本征正交分解方法对缸内湍流场数据库进行了深度加工,根据湍流场涡团结构含能量进行分解,有效实现了大尺度拟序结构和小尺度随机脉动涡团的分离,为研究拟序结构和其他不同尺度涡团特性提供了便利。另外,计算结果还表明,进气冲程阶段的进气射流主导着缸内早期整体流动形态,产生的大尺度拟序结构涡团在随后的过程中不断破碎成小尺度涡团,并伴随着能量级联现象的发生,之后缸内流场会逐渐趋于各向同性。 相似文献
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利用CFD三维数值模拟软件模拟了1台缸内直喷汽油机的进气及压缩过程,分析比较了不同最大气门升程及进气正时下缸内流场的变化规律。结果表明:减小最大气门升程可以使进气行程中缸内气体的速度及湍动能显著增加,但在压缩末期的滚流比要略小;在小气门升程下,进气门早开或者晚开都会使得进气过程的湍动能显著增加,在距上止点5mm,10 mm,15 mm的3个横截面上,早开和晚开进气门会使最大平均湍动能分别增加28.29%和43.47%,20.7%和40.81%,23.07%和49.58%,但在压缩后期间,进气门早开或者晚开时对缸内的平均湍动能影响不大;在小气门升程下,进气门的开启时间对压缩末期湍动能的分布有较大的影响,早开或者晚开进气门会使缸内的湍动能趋于一致。 相似文献
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对某柴油机螺旋进气道进行传统的气道稳流试验,得到了涡流比和流量系数。在与试验条件对等的边界条件下,应用仿真软件FIRE建立了气道的三维仿真模型,对不同气门升程下进气道内的流场进行了CFD计算;对比试验与计算的结果,两者吻合良好。结果表明,仿真计算省时,成本低,便于方案对比,可以获得气道内的流场分布规律;在柴油机螺旋进气道设计开发与性能评价中具有实用价值。 相似文献
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《JSAE Review》1996,17(4):423-428
In recent years, global environmental preservation and energy savings have become primary objectives even for truck engines. The 3RZ-FE engine, newly developed to succeed the 22R-E engine, is an in-line 4-cylinder 2.7-liter gasoline engine. With such features as 16-valve DOHC, well tuned intake system and a pair of balance shafts built into the cylinder block, this engine provides high performance, low fuel consumption, low exhaust emissions, low noise and vibration and high reliability. 相似文献
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原HS125GY车所配化油器为柱塞式PZ26,与普通两气门125 mL发动机相当,采用四气门设计的目的是要提高进气填充效率,但PZ26化油器实际上却限制了发动机的进气效率.应匹配大口径化油器、进气管、空滤器来提高进气效率空间,按RX125进气口等效直径匹配化油器、进气管和低阻力系数空滤器. 相似文献
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C. H. Lee 《International Journal of Automotive Technology》2017,18(2):317-325
CFD simulations of spray tip penetration with the standard KIVA3V, ‘original gas jet’ and ‘Normal gas jet profile with breakup length formula’ (NGJBL) spray models were performed to investigate the effects of nozzle orifice size and ambient gas density combinations on the spray penetration. The accuracy of the CFD simulation results was estimated by comparing them with available experimental data. The ambient gas density was varied in 12 kg/m3 intervals from 12 to 69 kg/m3 for each nozzle orifice diameter. The nozzle orifice diameters used were 119, 140, 183 and 206 mm. A total of 20 cases in the CFD simulations were considered with combinations of the 4 nozzle orifice diameters and 5 ambient gas densities. CFD simulations with the NGJBL spray model were more accurate than those with either the standard KIVA3V or gas jet spray models as the nozzle orifice diameter and ambient gas density was increased. The NGJBL and original gas jet model is more effective in predicting the spray tip penetration near the nozzle tip region. 相似文献
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