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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Multiple Combustion Stages Inside a Heavy-Duty Diesel Engine Retrofitted to Natural- Gas Spark-Ignition Operation
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Multiple Combustion Stages Inside a Heavy-Duty Diesel Engine Retrofitted to Natural- Gas Spark-Ignition Operation

机译:重型柴油发动机内的多个燃烧级,改装为天然气火花点火操作

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Converting existing diesel engines to natural-gas (NG) spark-ignition (SI) operation can reduce the dependence on oil imports and increase energy security. NG-dedicated conversion can be achieved by the addition of a gas injector in the intake manifold and of a spark plug in place of the diesel injector. Previous studies indicated that lean-burn NG inside the traditional diesel chamber (i.e., a bowl-in-piston geometry) is a two-stage combustion (i.e., a fast burn inside the bowl followed by a slower burn inside the squish). However, a triple-peak apparent heat release rate (AHRR) was seen at specific operating conditions (e.g., advanced spark timing (ST) at medium load and engine speed), suggesting that one of the two combustion stages may separate again. Specifically, the burn inside the squish region divided in two events before and after top dead center (TDC). This was due to the different flow motion inside the squish during the compression stroke compared to the one in the expansion stroke, which affected the combustion environments. The result was the apparition of two close peaks in pressure trace, which suggest larger gradients in pressure and temperature than at a more delayed ST. In addition, the phasing and magnitude of three peaks of the heat release changed cycle-to-cycle. As an advanced ST is the usual strategy used in lean-burn SI combustion, understanding phenomena such as the one presented here can be important for reducing engine-out emissions and increase engine efficiency.
机译:将现有的柴油发动机转换为天然气(NG)火花点火(SI)操作可以减少对石油进口的依赖并提高能源安全性。 NG专用转换可以通过在进气歧管中添加气体喷射器和代替柴油喷射器的火花塞来实现。先前的研究表明,传统柴油室内的稀燃NG(即活塞碗形)是两阶段燃烧(即在碗体内进行快速燃烧,然后在南瓜内进行较慢的燃烧)。但是,在特定工况下(例如,中等负载和发动机转速下的提前点火正时(ST)),出现了三峰表观放热率(AHRR),这表明两个燃烧阶段之一可能会再次分离。具体而言,挤压区内部的燃烧分为上死点(TDC)前后的两个事件。这是由于在压缩冲程期间壁球内部的流动运动与膨胀冲程中壁球中的不同,从而影响了燃烧环境。结果是在压力曲线中出现了两个接近的峰,这表明压力和温度的梯度要比延迟时间更短。另外,放热的三个峰值的相位和幅度在每个周期之间变化。由于先进的ST是稀薄燃烧SI燃烧中常用的策略,因此了解诸如此处介绍的现象对于减少发动机废气排放并提高发动机效率可能很重要。

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    《Journal of Engineering for Gas Turbines and Power 》 |2020年第2期| 021018.1-021018.7| 共7页
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    Mem. ASME Center for Alternative Fuels Engines and Emissions (CAFEE) West Virginia University Morgantown WV 26506;

    Mem. ASME Center for Alternative Fuels Engines and Emissions (CAFEE) West Virginia University Morgantown WV 26506-6106 Center for Innovation in Gas Research and Utilization (CIGRU) West Virginia University Morgantown WV 26506-6106;

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