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COMBUSTION OF NORMAL AND LOW CALORIFIC FUELS IN HIGH TEMPERATURE AND OXYGEN DEFICIENT ENVIRONMENT

机译:高温和缺氧环境中正常和低热值燃料的燃烧

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Combustion characteristics of two different gaseous fuels (a low calorific value fuel and methane fuel) have been examined using high temperature and low oxygen concentration combustion air. The momentum flux ratio between the fuel jet and the combustion airflow was kept constant to provide similarity in mixing between the different experimental cases to understand the role of fuel jet property on combustion. Direct flame photography, 2-D Particle image velocime-try (PIV), Light Emission Spectroscopy and chemiluminescent NO_X analyzer was used as the diagnostics. These diagnostics allowed information on global flame features, mean and rms components of axial and radial velocity, axial strain rates and vorticity, the spatial distribution of combustion intermediate species, such as, OH and CH, and overall NO_X emission levels. The results indicate a slower mixing during high temperature air combustion with low calorific value fuel as compared to methane fuel. The results showed higher turbulence levels and higher axial strain rates for low calorific fuel jets as compared to methane fuel jet during the high temperature air combustion condition. This results in less intense (or mild) combustion conditions with the result of increased flame length and volume and lower NO_X emissions. Even for the normal methane fuel high temperature and oxygen deficient combustion conditions provided lower NO_X emission. Furthermore, the high temperatures obtained for methane combustion provided lower vorticity and axial strain rates than the low calorific value fuel due to the suppression of vortical structure formation from the stronger heat release. In the case of low calorific value fuel, higher fuel jet velocity into low-density high temperature air leads to longer jet length. This jet causes a local stagnation to the upstream cross-flow to create local higher value of turbulence levels immediately upstream of the jet. The spatial distribution of the flame generated radicals (OH and CH) revealed significant ignition delay of the LCV fuel jet and a far more uniform distribution of the intermediate species. The methane fuel jet showed a prolonged reaction zone and faster ignition at high temperature and oxygen deficient conditions when compared to normal temperature air combustion of methane.
机译:已经使用高温和低氧浓度的燃烧空气检查了两种不同的气态燃料(低热值燃料和甲烷燃料)的燃烧特性。燃料射流与燃烧气流之间的动量通量比保持恒定,以在不同实验情况之间的混合中提供相似性,以了解燃料射流特性对燃烧的作用。诊断方法包括直接火焰摄影,二维粒子图像测速(PIV),发光光谱和化学发光NO_X分析仪。这些诊断信息可提供有关整体火焰特征,轴向和径向速度的均值和均方根值,轴向应变率和涡度,燃烧中间物质(如OH和CH)的空间分布以及总NO_X排放水平的信息。结果表明,与甲烷燃料相比,高温空气燃烧期间与低热值燃料的混合更慢。结果表明,相比于高温空气燃烧条件下的甲烷燃料喷嘴,低热量燃料喷嘴的湍流水平更高,轴向应变率更高。这导致较弱的(或温和的)燃烧条件,结果是增加了火焰长度和体积,并降低了NO_X排放量。即使对于普通的甲烷燃料,高温和氧气不足的燃烧条件也可以降低NO_X排放。此外,由于抑制了较强的热释放而形成的旋涡结构,因此与低热值燃料相比,用于甲烷燃烧的高温提供的旋涡和轴向应变率更低。在低热值燃料的情况下,进入低密度高温空气的较高燃料喷射速度会导致更长的喷射长度。该射流引起上游错流的局部停滞,从而在射流上游立即产生湍流水平的局部较高值。火焰产生的自由基(OH和CH)的空间分布表明LCV燃料射流的显着点火延迟以及中间物质的分布更加均匀。与常温下的甲烷空气燃烧相比,甲烷燃料射流在高温和缺氧条件下显示出更长的反应区和更快的点火。

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