首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part D. Journal of Automobile Engineering >Premixed compression ignition combustion with various injector configurations in a heavy duty diesel engine
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Premixed compression ignition combustion with various injector configurations in a heavy duty diesel engine

机译:重型柴油机中具有各种喷射器配置的预混压缩点火燃烧

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Premixed compression ignition combustion was implemented using early injection timing and exhaust gas recirculation in a direct injection single cylinder diesel engine and was evaluated with respect to the injector configurations. A baseline injector with an injection angle of 146° and eight nozzle holes showed premixed compression ignition combustion at the injection timing of 40° crank angle before top dead centre among three distinct combustion regimes. The burn duration in premixed compression ignition combustion was shortest among the regimes. Premixed compression ignition combustion at an injection timing of 40° crank angle before top dead centre was achieved at an exhaust gas recirculation rate ranging from 0% to approximately 40%. Two different injector configurations were applied to investigate the effect of injection angle and the number of nozzle holes on premixed compression ignition combustion: one had an injection angle of 70° and eight nozzle holes and the other had an injection angle of 70° and 14 nozzle holes. These two injectors could implement premixed compression ignition combustion as well as the baseline injector under the injection timing and exhaust gas recirculation conditions. In case of both injectors with an injection angle of 70°, the indicated mean effective pressures for 8 and 14 nozzle holes increased by 26% and 11%, respectively, because of the increased fuel participating in combustion and the reduced negative work in premixed compression ignition combustion. On the other hand, the injector with an injection angle of 70° and 14 nozzle holes showed the lowest levels of hydrocarbon, carbon monoxide and smoke emissions, which decreased by 82%, 92% and 81%, respectively, in premixed compression ignition combustion. However, the nitrogen oxides emission for the injectors with eight and 14 holes increased by 82% and 68%, respectively, in premixed compression ignition combustion. Natural luminosity from an in-cylinder visualization reveals pool fire of fuel films on the base of the piston bowl when both injectors had a narrow injection angle. For the injector with an injection angle of 70° and eight nozzle holes, a more vigorous pool fire at an exhaust gas recirculation rate of 0% is attributed to a larger amount of fuel film. At an exhaust gas recirculation rate of 40%, however, the portion of unburned fuel films increased the hydrocarbon and carbon monoxide emissions, and the rest of the diffusive pool fire can increase smoke emission surviving under a lack of oxygen. On the other hand, for the injector with an injection angle of 70° and 14 nozzle holes, the hydrocarbon and carbon monoxide emissions were maintained at lower levels due to less formation of fuel film and better air utilization.
机译:预混合压缩点火燃烧是在直喷单缸柴油机中使用提前喷射正时和废气再循环进行的,并针对喷射器配置进行了评估。在三种不同的燃烧方式中,具有146°喷射角和八个喷嘴孔的基准喷射器在上死点之前的40°曲轴转角喷射正时显示预混压缩点火燃烧。在这些方案中,预混压缩点火燃烧的燃烧持续时间最短。在上死点之前以40°曲柄角的喷射正时进行预混合的压缩点火燃烧,并且排气再循环率在0%到大约40%的范围内。应用了两种不同的喷油嘴配置,以研究喷油角度和喷嘴孔数对预混压缩点火燃烧的影响:一个喷油嘴角度为70°,喷油嘴为八个,另一个喷油嘴角度为70°,喷油嘴为14。孔。这两个喷射器可以在喷射正时和废气再循环条件下实现预混合压缩点火燃烧以及基线喷射器。在两个喷射器的喷射角均为70°的情况下,由于参与燃烧的燃料增加和预混合压缩中的负功减少,指示的8个和14个喷嘴孔的平均有效压力分别增加了26%和11%。点火燃烧。另一方面,具有70°喷射角和14个喷嘴孔的喷射器显示出最低的碳氢化合物,一氧化碳和烟气排放水平,在预混合压缩点火燃烧中分别减少了82%,92%和81% 。然而,在预混合压缩点火燃烧中,具有八个和十四个孔的喷射器的氮氧化物排放分别增加了82%和68%。缸内可视化的自然光度表明,当两个喷油嘴均具有狭窄的喷油角度时,燃料膜会在活塞碗的底部堆积。对于具有70°喷射角和八个喷嘴孔的喷射器,在较大的燃油再循环量的情况下,废气再循环率为0%时,更剧烈的池火。但是,在废气再循环率为40%的情况下,未燃烧的燃料膜部分会增加碳氢化合物和一氧化碳的排放,其余的扩散池火会增加烟气在氧气不足的情况下的存活率。另一方面,对于具有70°喷射角和14个喷嘴孔的喷射器,由于较少的燃料膜形成和更好的空气利用,碳氢化合物和一氧化碳的排放量保持在较低的水平。

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