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Experimental Investigation of Impacts of Injection Timing and Pressure on Combustion and Particulate Matter Emission in a Spray-Guided GDI Engine

机译:喷射引导GDI发动机注射时序对燃烧和颗粒物发射的影响的实验研究

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摘要

A detailed investigation of the impact of injection timing and injection pressure on combustion and particles of a spray-guided GDI engine was conducted, under different engine operating conditions. The results indicated that, more proportion of large particles were emitted when increasing engine load, and the peak of accumulation mode particles moved toward smaller size when rising engine speed. With retarding the injection timing, the in-cylinder pressure and heat release rate rose first and then dropped at 2000 rpm, but they continuously rose at lower or higher speed conditions. The total particles concentration curves at all cases showed a trend of U-shape, and the corresponding timing of the lowest particles concentration advanced as the engine speed or load increased. The minimum value of emitted particles first rose and then fell when increasing load at 2000 rpm conditions, and it continuously rose when increasing speed at 40 Nm conditions. Generally, injection pressure did no sensitively affect combustion process except that it showed a relatively strong impact at low load conditions. However, particulate matter could be effectively inhibited by elevating fuel pressure from 5.5 to 11.5 MPa at all cases. In detail, the total particles concentration continuously fell at low speed and mid speed-high load cases, but it showed a rose trend when further increase fuel injection pressure at mid speed-low load and high-speed conditions.
机译:在不同发动机操作条件下,进行了对喷射正时和注射压力对喷射引导GDI发动机燃烧和颗粒的影响的详细研究。结果表明,在增加发动机负荷时发射了更多比例的大颗粒,并且在上升发动机速度时,累积模式颗粒的峰值朝向更小的尺寸。延迟注射正时,缸内压力和热释放速率首先升高,然后以2000rpm掉落,但它们在较低或更高的速度下持续上升。所有情况下的总颗粒浓度曲线显示出U形的趋势,并且随着发动机速度或负荷增加的最低粒子浓度的相应定时增加。发射粒子的最小值首先升起,然后在增加2000 rpm条件下增加载荷时落下,并且当在40纳米条件下增加速度时它连续上升。通常,除了在低负荷条件下表现出相对强烈的影响之外,注射压力没有敏感地影响燃烧过程。然而,可以通过在所有情况下升高5.5至11.5MPa的燃料压力来有效地抑制颗粒物质。详细地,总颗粒浓度在低速和中速高负荷情况下连续下降,但在中速 - 低负载和高速条件下进一步提高燃料喷射压力时,它显示出玫瑰趋势。

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