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The Effect of Inlet Valve Timing and Engine Speed on Dual Fuel IMG-Diesel Combustion in a Large Bore Engine

机译:入口气门定时和发动机速度对大孔发动机双燃料IMG柴油燃烧的影响

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High load (18 bar IMEP) dual fuel combustion of a premixed natural gas/air charge ignited by directly injected diesel fuel was studied in a large bore gas engine. A nozzle design with low flow rate was installed to inject a small diesel volume (10.4 mm~3) equal an energetic amount of about two percent. The effect of compression end temperature on ignition and combustion was investigated using valve timings with early IVC (Miller) and maximum charging efficiency (MaxCC). Furthermore, the engine speed was reduced (1500 rpm to 1000 rpm) for the Miller valve timing to analyze the impact of the chemical time scale on the combustion process. During all experiments, the cylinder charge density was kept constant adjusting the intake, pressure and the resulting air mass flow. Unlike a typical reactivity-controlled compression ignition (RCCI) combustion process, the combustion phasing of the investigated pilot-ignited natural gas combustion was also sensitive to the injection timing besides the air-fuel equivalence ratio (AFER). As a consequence of the lower compression end temperature with Miller valve timing, the operating range of the AFER was shifted to significantly lower values (λ = 1.53 to 1.63) compared to MaxCC (λ = 1.88 to 2.08) and knocking combustion was no longer observed. Furthermore, the objective relation between the mass fraction burnt 50% (MFB50%) as a function of the start of energizing (SoE) at a constant air-fuel equivalence ratio was no longer valid, The experiments with MaxCC valve timing revealed that this behavior is not necessarily a characteristic of the pilot ignition. In fact, conditions inhibiting the ignition and engine knock result in loss of the one-to-one pairing between SoE and MFB50%. The reduction of the engine speed extended the lean misfire limit (λ = 1.53 to 1.75) and improved the engine start behavior.
机译:在大型孔内燃气发动机中研究了通过直接注入的柴油燃料点燃的预混天然气/空气电荷的高负荷(18bar IMEP)双燃料燃烧。安装低流量的喷嘴设计以注入小柴油体积(10.4mm〜3)等于大约2%的能量量。使用具有早期IVC(米勒)和最大充电效率(MAXCC)的阀门来研究压缩端温度对点火和燃烧的影响。此外,对于米勒阀正时,发动机速度降低(1500 rpm至1000rpm),以分析化学时间尺度对燃烧过程的影响。在所有实验期间,汽缸电荷密度保持恒定调节进气,压力和所得的空气质量流量。与典型的反应性控制压缩点火(RCCI)燃烧过程不同,除了空气燃料等效比(AFER)之外,研究的先导式天然气燃烧的燃烧相位对喷射正时也敏感。由于米勒气门正时的压缩端温度较低,与MAXCC(λ= 1.88至2.08)相比,Afer的操作范围变为显着较低的值(λ= 1.53至1.63),并不再观察到爆震燃烧。此外,在恒定空气 - 燃料当量比以激励(SOE)开始的函数的质量馏分烧伤50%(MFB50%)之间的物镜关系不再有效,MAXCC阀正时的实验表明这种行为不一定是试点点火的特征。事实上,抑制点火和发动机爆震的条件导致SOE和MFB50%之间的一对一配对。发动机速度的降低延伸了贫误重点(λ= 1.53至1.75),并改善发动机启动行为。

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