微型燃烧器扩展角对氢气/空气预混燃烧特性影响的模拟研究
Simulation Study on the Influence of Micro Burner Expansion Angle on Hydrogen/Air Premixed Combustion Characteristics
DOI: 10.12677/MOS.2021.101010, PDF, HTML, XML, 下载: 513  浏览: 1,546 
作者: 王 卓, 王 波*, 刘梦辉, 孙成喜：上海理工大学能源与动力工程学院，上海；俞志鹏, 姬 鹏：上海船用柴油机研究所，上海
关键词: 微型燃烧器；扩展角；入口速度；最高燃烧温度；Micro Burner； Expansion Angle； Inlet Velocity； Maximum Combustion Temperature
摘要: 基于建立的三维微型燃烧器模型，选用氢气体积分数为10%的预混气，对长度100 mm，扩展角分别为0˚、0.36˚、0.72˚的微型燃烧器内氢气/空气的预混燃烧过程进行模拟研究。研究发现，对方形微通道燃烧器，在相同的燃烧器长度、外壁边长和进口尺寸下，扩展角越大的燃烧器，速度极限范围越大。当入口速度较低时，扩展角越大，火焰传播速度越低，最高燃烧温度越高；当入口速度较高，燃气充分燃烧时，扩展角的大小对最高燃烧温度几乎没有影响。
Abstract: Based on the established three-dimensional model of the microburner, the premixed combustion process of hydrogen/air in a 100 mm long microburner with expansion angles of 0˚, 0.36˚ and 0.72˚ was simulated with 10% hydrogen volume fraction. It is found that for square micro-channel burners, with the same burner length, outer wall length and inlet size, the larger the burner ex-pansion angle, the larger the speed limit range. When the inlet velocity is low, the larger the spreading angle is, the lower the flame propagation velocity is, and the higher the maximum com-bustion temperature is; when the inlet velocity is high and the gas is fully burned, the expansion angle has little effect on the maximum combustion temperature.
文章引用：王卓, 俞志鹏, 姬鹏, 王波, 刘梦辉, 孙成喜. 微型燃烧器扩展角对氢气/空气预混燃烧特性影响的模拟研究[J]. 建模与仿真, 2021, 10(1): 93-106. https://doi.org/10.12677/MOS.2021.101010

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