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Implementation of a Dual Coil Ignition Strategy in a Split-Cycle Engine

机译:在分循环发动机中实现双线圈点火策略

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A Split-Cycle engine fueled with methane has been constructed and operated at the University of Windsor. A split-cycle engine consists of two interconnected cylinders working together to preform the four engine strokes. Cylinder 1 preforms intake and compression strokes while cylinder 2 is where combustion, expansion and exhaust occur. The connecting high pressure crossover passage is where methane is injected, resulting in a well pre-mixed air-fuel mixture. Transfer occurs to the combustion cylinder near TDC, resulting in intense small scale turbulence that leads to short combustion durations under 30°CA. Short durations are achieved despite low engine speeds of 850-1200 rpm, late combustion phasing and part loads. Of note is the lean limit of operation of the engine at the equivalence ratio Φ=85, which is high compared to other natural gas engines which have limits around Φ=0.6. The high levels of turbulence combined with a high amount of residual mass being trapped in the combustion cylinder are considered to be the limiting factor for the lean limit of operation. An extension of the lean limit is explored using a dual coil ignition strategy in which two coils are discharged through a single spark plug, increasing the amount of energy deposited to each kernel. Similar strategies have shown the effectiveness of increased energy in both highly turbulent and diluted mixtures. The normalized pressure ratio (PRN) method is used to acquire results for combustion phasing and cyclic variability. The dual coil strategy has been shown to be an effective way to extend the lean limit of operation of an engine in lean, dilute and turbulent conditions. The COV_(IMEP), COV_(LPP) and number of misfires decrease, indicating increased combustion stability. Equivalence ratio is extended to Φ=0.81. It can be used in scenarios where combustion in the lean condition is desired.
机译:用甲烷燃料的分流循环发动机已经在温莎大学建造和运营。分流循环发动机由两个与之一起工作以预制四个发动机冲程的互连汽缸组成。圆筒1预成型进气和压缩冲程,而气缸2是燃烧,膨胀和排气的地方。连接的高压交叉通道是注入甲烷的地方,导致井预混空气燃料混合物。转移发生在TDC附近的燃烧圆筒上,导致强烈的小规模湍流,导致30°下的燃烧持续时间短。尽管发动机速度为850-1200rpm,后期燃烧序列和部件载荷,但仍实现短持续时间。注意是在等效比φ= 85处的发动机的操作稀薄极限,其与具有围绕φ= 0.6限制的其他天然气发动机相比。与高量捕获在燃烧缸中的高量湍流结合的高水平湍流被认为是贫液限制的限制因素。使用双线圈点火策略探索贫极限的延伸,其中两个线圈通过单个火花塞排出,增加沉积在每个内核的能量的量。类似的策略表明了高度湍流和稀释的混合物中的能量增加的有效性。归一化压力比(PRN)方法用于获取燃烧相位和循环变异性的结果。双线线圈策略已被证明是扩展稀薄,稀释和湍流条件下发动机的贫尺寸的有效方法。 COV_(IMEP),COV_(LPP)和失火次数减少,表明燃烧稳定性增加。等效率扩展到φ= 0.81。它可以在需要贫态条件中的燃烧的情况下使用。

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