首页> 外文会议>ASME Internal Combustion Engine Division technical conference >INFLUENCE OF THE SPATIAL AND TEMPORAL INTERACTION BETWEEN DIESEL PILOT AND DIRECTLY INJECTED NATURAL GAS JET ON IGNITION AND COMBUSTION CHARACTERISTICS
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INFLUENCE OF THE SPATIAL AND TEMPORAL INTERACTION BETWEEN DIESEL PILOT AND DIRECTLY INJECTED NATURAL GAS JET ON IGNITION AND COMBUSTION CHARACTERISTICS

机译:柴油先导与直接喷射天然气射流之间的时空相互作用对点火和燃烧特性的影响

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In this paper, pilot-ignited high pressure dual-fuel (HPDF) combustion of a natural gas jet is investigated on a fundamental basis by applying two separate single-hole injectors to a rapid compression expansion machine (RCEM). A Shadowgraphy system is used for optical observations, and the combustion progress is assessed in terms of heat release rates. The experiments focus on the combined influence of injection timing and geometrical jet arrangement on the jet interaction and the impact on the combustion process. In a first step, the operational range for successful pilot self-ignition and transition to natural gas jet combustion is determined, and the restricting phenomena are identified by analyzing the shadowgraph images. Within this range, the combustion process is assessed by evaluation of ignition delays and heat release rates. Strong interaction is found to delay or even prohibit pilot ignition, while it facilitates a fast and stable onset of the gas jet combustion. Furthermore, it is shown that the heat release rate is governed by the time of ignition with respect to the start of natural gas injection - as this parameter defines the level ofpremixing. Evaluation of the time of gas jet ignition within the operability map can therefore directly link a certain spatial and temporal interaction to the resulting heat release characteristics. It is finally shown that controlling the heat release rate through injection timing variation is limited for a certain angle between the two jets.
机译:在本文中,通过将两个单独的单孔喷油器应用于快速压缩膨胀机(RCEM),从根本上研究了天然气喷射器的引燃高压双燃料(HPDF)燃烧。影印系统用于光学观察,并根据放热率评估燃烧过程。实验着重于喷射正时和几何射流布置对射流相互作用以及对燃烧过程的影响的综合影响。第一步,确定成功进行飞行员自燃和过渡到天然气喷射燃烧的操作范围,并通过分析阴影图图像来识别限制现象。在此范围内,通过评估点火延迟和放热率来评估燃烧过程。发现强烈的相互作用会延迟甚至禁止引燃器点火,同时它有助于快速稳定地喷射气体燃烧。此外,显示出相对于天然气注入的开始,放热率受点火时间的控制-因为该参数定义了预混合的水平。因此,在可操作性图内对气体喷射点火时间的评估可以将特定的时空相互作用直接与所产生的放热特性联系起来。最终表明,通过喷射正时变化来控制放热速率对于两个射流之间的某个角度是有限的。

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