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Investigation of Micro Pilot Combustion in a Stationary Gas Engine

机译:固定式燃气发动机微飞行员燃烧的研究

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The objective of this program was to obtain 35 percent brake thermal efficiency (BTE) based on tuel higher heating value with NO_x emission levels below 0.7 g/bhp-hr. The demonstration engine was a Superior 1706 rated at 400 hp at 1200 rpm. Three design alternatives were tested: two micro pilot prechamber (MPPC) configurations and one micro pilot open chamber configuration. THe results demonstrated that the micro pilot technology could achieve low emissions and high efficiency, depending on the design and implementations of the technology. One micro pilot prechamber configuration tested met the objectives of the program. The prechamber versions obtained lower NO_x levels than the open chamber version at equivalent efficiency. The data indicated that a better NO_x-BTE trade-off was obtained as the pilot quantity was decreased and as the air-fuel ratio was increased.
机译:该程序的目标是基于较高的热值(NO_x排放水平低于0.7 g / bhp-hr)获得35%的制动热效率(BTE)。示范发动机是Superior 1706,额定功率为1200 rpm,功率为400 hp。测试了三种设计替代方案:两种微型先导腔(MPPC)配置和一种微型先导开放腔配置。结果表明,取决于该技术的设计和实现,微飞行员技术可以实现低排放和高效率。测试的一种微型飞行员预燃室配置满足了该计划的目标。在相同的效率下,预燃室版本获得的NO_x水平低于开燃室版本。数据表明,随着引燃数量的减少和空燃比的增加,可以获得更好的NO_x-BTE权衡。

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