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Effect of high squish combustion chamber on simultaneous reduction of NO_x and particulate from a direct-injection diesel engine

机译:高鳞型燃烧室对直喷柴油发动机同时减少NO_X和颗粒的影响

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In this study it is tried to reduce NO_x and particulate emissions simultaneously in a direct-injection diesel engine based on the concept of two-stage combustion. At initial combustion stage, NO_x emission is reduced with fuel rich combustion. At diffusion combustion stage, particulate emission is reduced with high turbulence combustion. The high squish combustion chamber with reduced throat diameter is used to realize two-stage combustion. This combustion chamber is designed to produce strong squish that causes high turbulence. When throat diameter of the high squish combustion chamber is reduced to some extent, simultaneous reduction of NO_x and particulate emissions is achieved with less deterioration of fuel consumption at retarded injection timing. Further reduction of NO_x emission is realized by reducing the cavity volume of the high squish combustion chamber. Analysis by endoscopic high-speed photography and CFD calculation describes the experimental results. Endoscopic photography shows that in the high squish combustion chamber, the high luminosity flame is observed beneath the squish lip until middle diffusion combustion stage. However, in the original toroidal combustion chamber, whole chamber is filled with brilliant flame from early combustion stage. The CFD calculation shows that in the high squish chamber, strong turbulence caused by intensified squish and high swirl produces a complex air motion with which spirally rotting mixture forms beneath the squish lip in the cavity. When the mixture burns, violent expansion flow toward the cavity center occurs, a part of burned gas is rolled back into the mixture again. It is also found that in the high squish combustion chamber fuel-rich mixture burns mainly in the cavity, and less unburned fuel spreads out to the clearance volume. The results of the CFD calculation agree with those of the endoscopic photography. It is suggested that strong swirl and squish obtained by combustion chamber geometry produce fuel-rich and high-turbulence combustion, which results in the reduction of NO_x and particulate emissions.
机译:在本研究中,试图基于两级燃烧的概念,在直喷柴油机中同时减少NO_X和微粒排放。在初始燃烧阶段,NO_X排放减少了富含燃料的燃烧。在扩散燃烧阶段,用高湍流燃烧减少颗粒发射。具有降低的喉部直径的高鳞屑腔用于实现两级燃烧。该燃烧室设计用于产生强烈的卷绕导致高湍流。当高鳞状燃烧室的喉部直径在一定程度上减少时,通过在延迟注射正时减少燃料消耗的劣化来实现NO_X和颗粒排放的同时降低。通过减小高鳞屑燃烧室的腔体积来实现NO_X发射的进一步减少。内窥镜高速摄影和CFD计算分析描述了实验结果。内窥镜摄影显示,在高鳞屑燃烧室中,在鳞状唇缘下观察到高亮度火焰,直到中间扩散燃烧阶段。然而,在原始环形燃烧室中,全室充满了早期燃烧阶段的亮起。 CFD计算表明,在高鳞状腔室中,由强化鳞状和高旋流引起的强烈湍流产生复杂的空气运动,其中螺旋旋转混合物在腔内的鳞状唇下方形成。当混合物燃烧时,发生朝向腔中心的剧烈膨胀流动,将一部分燃烧的气体再次卷回混合物。还发现,在高鳞状燃烧室燃料富燃烧的混合物主要在腔体中燃烧,并且较少的未燃烧的燃料扩散到间隙体积。 CFD计算结果与内窥镜摄影的结果一致。建议通过燃烧室几何形状获得的强旋流和鳞片产生富含燃料和高湍流燃烧,这导致NO_X和颗粒排放的减少。

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