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COMBUSTION OF LOW CALORIFIC FUELS IN HIGH TEMPERATURE OXYGEN DEFICIENT ENVIRONMENT

机译:高温缺氧环境中低热值燃料的燃烧

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Combustion characteristics of two different gaseous fuels (a low calorific value fuel and methane fuel)have been examined. The experiments are performed in an experimental high temperature air combustionfacility using gas fuel jet injected to a transverse flow of high temperature combustion air having lowerthan normal oxygen concentration. The composition and temperature of the combustion air flow can becontrolled and varied in order to simulate phenomena that occur in high temperature air combustionconditions. The momentum flux ratio between the fuel jet and the combustion air flow was kept constantto provide similarity between the different experimental cases and to understand the role of fuel jetproperty on mixing and combustion. Direct flame photography was used to obtain information on theglobal flame features. A 2-D Particle image velocimetry (PIV) was used to provide information on theinstantaneous flow field for the different cases investigated. This diagnostics allowed information onmean and rms axial and radial velocity, axial, radial and total strain rates and vorticity. The NOXemissions levels were also recorded.The results provide detailed information of the fluid dynamics that occurs during high temperature aircombustion conditions. The results indicate a slower mixing during high temperature air combustion witha low calorific value fuel as compared to methane fuel. The results showed higher turbulence levels andhigher axial strain rates for low calorific fuel jets as compared to methane fuel jet during the hightemperature air combustion condition. This leads to less intense (or mild) combustion conditions toprovide increased flame length and volume and lower NOX emissions for the low calorific value fuel.Even for the normal methane fuel high temperature air combustion conditions mean reduced emissions ofNOX. In contrast the high temperatures obtained for methane combustion leads to lower vorticity andaxial strain rates than the low calorific value fuel as the stronger heat release suppresses the formation ofvortical structures. In the case of low calorific value fuel, higher fuel jet velocity into low density hightemperature air leads to prolonged jet length. This jet causes a local stagnation to the upstream cross flowto create local higher value of turbulence levels immediately upstream of the jet. In this upstream regionof the jet, the turbulence levels, axial strain rates, and vorticity are much higher for the low calorific valuefuel than methane fuel.
机译:两种不同气态燃料(低热值燃料和甲烷燃料)的燃烧特性 已经检查过了。实验是在实验性高温空气燃烧中进行的 使用气体燃料射流的设备喷射到高温燃烧空气的横向流中,具有较低的 高于正常的氧气浓度。燃烧气流的成分和温度可以是 为了模拟高温空气燃烧中发生的现象而对其进行控制和变化 情况。燃料射流和燃烧空气流之间的动量通量比保持恒定 提供不同实验案例之间的相似性,并了解燃油喷射的作用 混合和燃烧的特性。直接火焰摄影被用来获取有关火星的信息。 全局火焰特征。二维粒子图像测速(PIV)用于提供有关 针对不同情况的瞬时流场进行了研究。此诊断允许有关以下内容的信息 平均和均方根轴向和径向速度,轴向,径向和总应变率和涡度。氮氧化物 还记录了排放水平。 结果提供了在高温空气中发生的流体动力学的详细信息 燃烧条件。结果表明,高温空气燃烧过程中的混合速度较慢, 与甲烷燃料相比,低热值燃料。结果显示出更高的湍流度和 低热量燃料喷射时的轴向应变率比高热量燃料喷射时的甲烷燃料喷射高 温度空气燃烧条件。这导致较弱的(或温和的)燃烧条件 为低热值燃料提供增加的火焰长度和体积,以及更低的NOX排放量。 即使对于普通的甲烷燃料,高温空气燃烧条件也意味着减少了二氧化碳的排放。 氮氧化物相反,甲烷燃烧所获得的高温导致较低的涡度和 轴向应变率低于低热值燃料,因为更强的热量释放抑制了燃料的形成 旋涡结构。在低热值燃料的情况下,较高的燃料喷射速度变为低密度高 高温空气会导致射流长度延长。该射流对上游错流造成局部停滞 在射流上游直接产生更高的湍流水平值。在这个上游地区 对于低热值,湍流水平,轴向应变率和涡度要高得多 燃料比甲烷燃料。

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