共查询到19条相似文献,搜索用时 125 毫秒
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高温空气燃烧技术具有高效节能和低NOx排放等多重优越性,是一种新型燃烧技术。为了深入研究高温空气燃烧机理和低氮氧化物排放特性,将湍流N—S方程与扩散燃烧模型和热力型NO生成模型相结合,研究了低氧浓度条件下,燃烧参数,如燃气供应量,过量空气系数,进口空气预热温度以及进口空气氧含量对燃烧的影响,为发展高温空气燃烧技术提供了理论依据。 相似文献
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高温空气燃烧技术的特点及其应用前景 总被引:3,自引:1,他引:2
高温空气燃烧技术(HTAC)是九十年代初在日本开发的一项新的燃烧技术,该项技术具有节约燃烧、低NOx排放、热利用率高和减设备尺寸等特点。分析了HTAC的火焰温度分布特征及其可降低NOx排放的原理。高炉煤气、焦炉煤气及94.5%高炉煤气与5.5%焦炉煤气的混合煤气应用于HTAC技术的理论计算结果表明,理论燃烧温度随着预热空气和燃气温度的升高而升高,因此HTAC技术可燃用传统燃烧方式不能使用的低热值燃气。此外,空气、燃气双预热可奖排烟温度将得更低,热利用率提高更高。最后,指出了在燃油、燃气锅炉及煤(或可燃固体废弃物)气化系统中采用HTAC技术的可能性。 相似文献
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高温低氧燃烧技术的关键设备--蜂窝状蓄热式热交换器的优化设计 总被引:1,自引:0,他引:1
讨论了高温空气燃烧技术的优势,即预热空气的节能效果及低NOx生成特性;而高效热交换器是高温低氧空气燃烧技术的一个关键,计算了空气、烟气在其关键设备——蜂窝状蓄热式热交换器中的换热系数、阻力及总传热系数,证实了其在热能回收利用方面的优越性。 相似文献
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烟气再循环实现低NOx排放的实验研究 总被引:1,自引:1,他引:0
实现高温空气燃烧技术的关键是控制燃烧区内的含氧体积浓度.建立了一套小型高温空气燃烧系统.采用炉外烟气再循环实现高温空气燃烧所需要的低氧环境.对烟气再循环对高温空气燃烧NOx排放特性的影响进行了实验研究,并分析了燃烧室的温度分布情况,总结了NOx及燃烧特性随烟气再循环率的变化的规律. 相似文献
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流化床中高水分煤的燃烧与排放试验研究 总被引:1,自引:0,他引:1
通过在一小型流化床中进行高水分煤的燃烧与排放的试验研究,表明水分含量和空气-燃料比对于高水分煤的燃烧与排放有较大影响。随着水分增加,流化床床温下降,NOx、SOx排放量也下降。空气-燃料比存在一最佳值,这时床温最高,而偏离此值,床温下降,随着空气量的增加,NOx、SOx排放量也增加。当空气-燃料比变化时,燃烧干煤与燃烧高水分煤有着类似的试验结果。 相似文献
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研究空气分级和废气循环燃烧等方式对油燃烧中NOx 生成的影响。实验发现 :分级燃烧对于燃料氮的转化有抑制作用 ,而且对含氮量较高的油燃料效果较明显 ,不论燃烧器功率如何 ,降低一次风率总使得NOx 的生成量减少 ;当一次风率占总过量空气系数的 50 %左右时 ,燃料氮的转化率存在一个最小值 ,而后随着一次风率的提高而增大并趋于一常数 ;增加废气循环率能降低油燃烧中NOx 的生成量 ,而且对于含氮量较低的油效果较明显 ,随着废气循环率增加 ,NOx 生成量的降幅趋缓并带来火焰稳定问题 ,因此存在有一个最佳废气循环率 ;废气循环燃烧会增大燃料氮的转化率 ,而且在一次风率较小情况下表现明显 相似文献
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Hirotatsu Watanabe Yoshikazu Suwa Yohsuke Matsushita Yoshio Morozumi Hideyuki Aoki Shoji Tanno Takatoshi Miura 《Energy Conversion and Management》2008,49(6):1530-1537
The present paper describes a numerical investigation of spray combustion in a jet mixing type combustor. In this combustor, kerosene spray was injected with a pressure atomizer, and high speed combustion air was introduced towards the spray flow through some inlet air nozzles to improve mixing of the spray and the air. In the numerical simulation, the conservative equations of mass, momentum and energy in the turbulent flow field were solved in conjunction with the k–ε two equation turbulence model. The effects of the diameter and the number of air inlet nozzles on the combustion behavior and NO emission were numerically investigated. When the diameter of the inlet air nozzle decreased from 8 to 4 mm, the calculated NO mole fraction in the exhaust gas was drastically decreased by about 80%. An increase in the inlet velocity resulted in improvement of the mixing of the spray and the air, and hence, the high temperature region where thermal NO was formed became narrow. As a result, the exhaust NO mole fraction decreased. Furthermore, a decrease in exhaust NO mole fraction was explained by a decrease in the residence time in the high temperature region above 1800 K. 相似文献
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Colorless distributed combustion (CDC) has been demonstrated to provide ultra-low emission of NOx and CO, improved pattern factor and reduced combustion noise in high intensity gas turbine combustors. The key feature to achieve CDC is the controlled flow distribution, reduce ignition delay, and high speed injection of air and fuel jets and their controlled mixing to promote distributed reaction zone in the entire combustion volume without any flame stabilizer. Large gas recirculation and high turbulent mixing rates are desirable to achieve distributed reactions thus avoiding hot spot zones in the flame. The high temperature air combustion (HiTAC) technology has been successfully demonstrated in industrial furnaces which inherently possess low heat release intensity. However, gas turbine combustors operate at high heat release intensity and this result in many challenges for combustor design, which include lower residence time, high flow velocity and difficulty to contain the flame within a given volume. The focus here is on colorless distributed combustion for stationary gas turbine applications. In the first part of investigation effect of fuel injection diameter and air injection diameter is investigated in detail to elucidate the effect fuel/air mixing and gas recirculation on characteristics of CDC at relatively lower heat release intensity of 5 MW/m3 atm. Based on favorable conditions at lower heat release intensity the effect of confinement size (reduction in combustor volume at same heat load) is investigated to examine heat release intensity up to 40 MW/m3 atm. Three confinement sizes with same length and different diameters resulting in heat release intensity of 20 MW/m3 atm, 30 MW/m3 atm and 40 MW/m3 atm have been investigated. Both non-premixed and premixed modes were examined for the range of heat release intensities. The heat load for the combustor was 25 kW with methane fuel. The air and fuel injection temperature was at normal 300 K. The combustor was operated at 1 atm pressure. The results were evaluated for flow field, fuel/air mixing and gas recirculation from numerical simulations and global flame images, and emissions of NO, CO from experiments. It was observed that the larger air injection diameter resulted in significantly higher levels of NO and CO whereas increase in fuel injection diameter had minimal effect on the NO and resulted in small increase of CO emissions. Increase in heat release intensity had minimal effect on NO emissions, however it resulted in significantly higher CO emissions. The premixed combustion mode resulted in ultra-low NO levels (<1 ppm) and NO emission as low as 5 ppm was obtained with the non-premixed flame mode. 相似文献
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