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Impact of the pre-chamber nozzle orifice configurations on combustion and performance of a Natural Gas Engine

机译:燃烧室前喷嘴孔口结构对天然气发动机燃烧和性能的影响

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摘要

In this study, a pre-chamber was designed to form near stoichiometric mixture and provide multiple turbulent flame jets to ignite the lean mixture and accelerate the combustion in the main combustion chamber for a natural gas engine. A CFD simulation was employed to investigate the impact of the pre-chamber nozzle configurations on flow and combustion processes inside the engine, as well as on the performance of the engine. Various configurations were investigated, including orifice number of 4 to 8 and orifice diameter ranging from 1.6 m to 2.9 mm. A non-dimensional parameter, β, was used to characterize the relative flow area of these configurations. The numerical results indicate that, for a given nozzle flow area, among the design of different orifice numbers, the 6-orifice design can obtain the optimal combustion and engine performance. Otherwise, a design of more orifices leads to slower flame penetrating speed in the main-chamber, and the design of less orifices leads to slower circumferential flames propagations in the main-chamber. Moreover, for a 6-orifice pre-chamber, the optimal orifice diameter was found to be 2.0 mm, corresponding to a β value of 0.3. A design of larger diameters leads to slower penetrating for the flame jets and insufficient radial flame propagations in the main-chamber, while a design of relatively smaller orifice diameters leads to insufficient circumferential flames propagations in the main-chamber. Additionally, for the engine performance, all the pre-chamber designs improve the indicated efficiency and reduce the NOx emission. Especially, the design of 6-orifice with diameter of 2.0 mm achieves a 35.0% increase of indicated thermal efficiency and a 78.0% reduction of NOx emission compared to the prototype engine.
机译:在这项研究中,设计了一个预燃烧室,以形成接近化学计量的混合物,并提供多个湍流火焰喷射器来点燃稀薄混合物,并加速天然气发动机主燃烧室中的燃烧。 CFD仿真用于研究预燃室喷嘴配置对发动机内部的流动和燃烧过程以及发动机性能的影响。研究了各种构造,包括孔数为4至8,孔口直径为1.6 m至2.9 mm。使用无量纲参数β来表征这些配置的相对流动面积。数值结果表明,对于给定的喷嘴流通面积,在不同孔数的设计中,六孔设计可以获得最佳的燃烧和发动机性能。否则,更多孔的设计会导致主腔室内的火焰穿透速度变慢,而较小孔的设计会导致主腔内周向火焰传播的速度变慢。而且,对于6孔的预燃室,发现最佳的孔直径是2.0mm,对应于0.3的β值。较大直径的设计导致火焰喷射的穿透较慢,并且主腔室中的径向火焰传播不足,而孔口直径相对较小的设计导致主腔室中的周向火焰传播不足。此外,对于发动机性能,所有的前室设计均提高了指示的效率并减少了NOx排放。特别是与原型发动机相比,直径为2.0 mm的6孔设计可提高指示热效率35.0%,减少NOx排放78.0%。

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