排气弯管结构参数对回流环形燃烧室出口温度分布的影响  

The Influence of Geometric Parameters of Transition Duct on Exit Pattern Factor of Reverse Flow Annular Combustor

作　　者：刘存喜[1,2] 段冬霞[1,2] 毛艳辉[1,2] 崔玉峰[1] 徐纲[1] 

机构地区：[1]中国科学院工程热物理研究所,北京100190 [2]中国科学院研究生院,北京100190

出　　处：《燃气轮机技术》2011年第4期17-21,共5页Gas Turbine Technology

基　　金：国家自然科学基金(50806077和50706054)

摘　　要：本文采用标准k-ε湍流模型进行弯管准三维轴对称和三维数值模拟,研究弯管几何结构对回流环形燃烧室出口温度分布的影响。结果表明,弯管中心轴线长度和进出口面积收敛比对出口温度分布有重要的影响,压力损失系数的影响次之。得到了弯管进出口温度分布系数的比值与压力损失系数、无量纲中心轴线长度和进出口面积收敛比的函数关系,所得结果可为满足出口温度分布系数的回流环形燃烧室排气弯管结构的优化设计提供有用的依据。The standard k-ε turbulence model is used to study the influence of geometric parameters of transition duct on the exit pattern factor of reverse annular combustor,both for quasi-three-dimension and three-dimension.The results show that,the length of central axis and the area ratio between inlet and outlet of transition duct are of paramount importance on the exit pattern factor of combustor,the effect of pressure-loss factor on exit pattern factor is less important.Furthermore,the correlation between ratio of pattern factor from inlet to outlet of the transition duct and pressure-loss factor,dimensionless length of central axis,area ratio between inlet and outlet of the duct is obtained.The results can be used to guide the design of transition duct of reverse flow annular gas turbine combustors in which exit pattern factor can be satisfying.

关 键 词：回流燃烧室 燃气轮机 排气弯管 几何结构 温度分布系数 

分 类 号：V231.2[航空宇航科学与技术—航空宇航推进理论与工程]