模拟稀燃天然气发动机的定容室分室结构对放热速率的影响

Y. Nada, Y. Kidoguchi, Yuto Yamashita, R. Furukawa, Ryu Kaya, Hideaki Nakano, S. Kobayashi
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引用次数: 1

摘要

分燃烧室是保证压缩天然气发动机在稀薄燃烧条件下稳定运行的重要装置。在我们之前的研究中,我们将一种分室喷射系统应用于CNG发动机,该系统将单个喷油器和火花塞安装在一个小的分室中。本研究的目的是研究副燃烧室结构对主燃烧室放热的影响。在压力为2.3 MPa、整体等效比为0.6的条件下,研究了11种不同喷嘴数量、喷嘴直径和子室容积的子室。当采用较小喷嘴的分室时,燃烧后的燃气射流侵彻速度增大。此外,随着子室体积的增大,速度也随之增大。燃烧后气体射流的高速穿透缩短了初始火焰发展的时间。这是因为高温燃烧后的气体迅速到达主室侧壁,并立即点燃主室中存在的稀薄混合物。因此,燃烧持续时间,直到热释放达到90%也缩短。另一方面,不同喷嘴数的子腔射流速度差较小。为了预测侵彻速度,提出了基于分腔体积、喷管直径和喷管数量的经验公式。由公式计算得到的射流强度与燃烧周期的持续时间和燃烧后射流的穿透速度有关。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Effects of Sub-Chamber Configuration on Heat Release Rate in a Constant Volume Chamber simulating Lean-burn Natural Gas Engines
Sub-chamber is a useful device with regard to sustaining stable operation of compressed natural gas (CNG) engines under lean burn conditions. In our previous studies, we applied a sub-chamber injection system to CNG engines, in which a single injector and a spark plug are mounted in a small sub-chamber. The aim of this study is to investigate the effect of the sub-chamber configuration on heat release in the main combustion chamber. 11 types of sub-chamber with different nozzle number, nozzle diameter, and sub-chamber volume were examined under a condition that pressure is 2.3 MPa, and global equivalence ratio is 0.6. When the sub-chamber with smaller nozzles are used, the penetration velocity of burned gas jet increases. In addition, the velocity also increases with an increasing sub-chamber volume. The high-speed penetration of burned gas jet shortens the period of initial flame development. This is because the high-temperature burned gas quickly reaches to side wall of main chamber, and immediately ignites lean mixtures existing in the main chamber. Consequently, combustion duration time until heat release reaches 90 % is also shortened. On the other hand, the velocity difference between the jets from sub-chambers with different nozzle numbers is small. To predict the penetration velocity, we proposed an empirical formula based on the volume, nozzle diameter and nozzle number of sub-chamber. The jet intensity evaluated from the formula shows correlations with duration times of combustion periods as well as penetration velocities of burned gas jets.
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