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Numerical study of HCCI combustion in diesel engines using reduced chemical kinetics of n-heptane with multidimensional CFD code

机译:利用多维CFD码降低化学动力学柴油机HCCI燃烧的数值研究

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The homogeneous charge compression ignition (HCCI) is one of the alternatives to reduce significantly engine emissions for the future regulations. The combustion process in HCCI engines does not involve flame propagation or flame diffusion as in conventional internal combustion engines. Many studies have confirmed that during this mode the combustion process is mainly controlled by chemical kinetics. However, a coupled CFD and detailed chemistry simulation requires substantial memory and CPU time which may be very difficult with current computer capabilities. Thus a reduced mechanism is required to simulate the engine cycle during this operating mode to achieve more accurate analysis. In this study reduced chemistry was used with an engine CFD code combustion (Star-CD/Kinetics) to study combustion process in homogeneous charge compression ignition (HCCI) engines. The Chemkin code was used at first to develop a reduced autoignition model for n-heptane using a systematic sensitivity analysis approach. The reduced mechanism with 37 species and 61 reactions reproduces the ignition delay times of the mixture over a wide range of engine operating conditions (inlet pressure and temperature, air-fuel ratio, engine speed, compression ratio and EGR rate). The results obtained have been validated by comparison with detailed mechanisms developed by Lawrence Livermore National Laboratory, Chalmers University and the shock tube experiments of Ciezki and Adomeit. The comparison shows that the reduced mechanism behaves in the same way as these detailed models for the description of the two stages phenomenon (cool flame zone followed by main ignition), but also for the temperature and pressure inside the cylinder. The reduced reaction scheme has been implemented in Star-CD/Kinetics CFD code. As the computational time for the original mesh (3D - 38000 cells) was too high on a work station, we have used a simplified mesh (2D - 700 cells) with only 14 hours computational time which reproduced similar results. With the simplified mesh and the reduced reaction scheme, the numerical simulations in homogeneous mode show that heat release is very steep whatever the operating conditions (equivalence ratio, EGR rate, inlet pressure) which is in agreement with the massive self-ignition of the homogeneous charge. The simulations with different EGR rates confirm that the dilution by EGR delays the ignition timing when the gas temperature is not changed.
机译:均质充量压燃(HCCI)是替代显著减少未来的法规发动机排放的一个。在HCCI发动机中的燃烧过程不涉及火焰传播或火焰扩散如在常规的内燃机。许多研究已经证实,这种模式在燃烧过程中主要是由化学动力学控制。然而,耦合CFD和详述化学模拟需要大量的存储器和CPU时间,其可以是与当前的计算机能力非常困难。因此减小机构需要此操作模式期间,以模拟发动机循环以获得更准确的分析。在这项研究中还原的化学性质是与发动机CFD代码燃烧(STAR-CD /动力学)研究燃烧过程在均质充量压缩点火(HCCI)发动机中使用。所述CHEMKIN代码起初被用来建立通过系统的灵敏度分析方法为正庚烷减少自燃模型。与37种和61个反应的降低机构在宽范围的发动机操作条件(入口压力和温度,空气燃料比,发动机速度,压缩比和EGR率)再现该混合物的点火延迟时间。得到的结果是由与劳伦斯利弗莫尔国家实验室,查尔姆斯理工大学和Ciezki和Adomeit的激波管实验制定了详细的机制比较有效。比较结果显示,在以同样的方式减小的机制表现为对于两个阶段现象的描述(冷焰区,接着主点火),而且对于温度和压力的气缸内这些详细的模型。降低的反应方案已在STAR-CD /动力学CFD代码得到执行。作为计算时间的原始目(3D - 38000个细胞)过高工作站上,我们已经使用的简化目(2D - 700个细胞)与该再现类似的结果仅14小时计算时间。与简化网格和减少的反应方案中,在均相模式显示的数值模拟的热量释放很陡的任何操作条件(当量比,EGR率,入口压力),这是在协议与所述均匀的大量自点火收费。用不同的EGR率的仿真确认稀释由EGR延迟点火正时的气体温度也不会改变。

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