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驻涡燃烧室驻涡区涡系特点数值模拟
引用本文:彭春梅,何小民,金 义.驻涡燃烧室驻涡区涡系特点数值模拟[J].航空发动机,2013,39(1):51-55.
作者姓名:彭春梅  何小民  金 义
作者单位:南京航空航天大学能源与动力学院,南京,210016
摘    要:为深入了解驻涡燃烧室凹腔内流场的涡系分布特性,采用FLUENT对不同驻涡区前进口堵塞比和不同燃烧室入口速度的驻涡区流场进行计算,分析典型截面压力场和流线图,研究驻涡区涡系特点.结果表明:不同纵截面旋涡特点不同,主流被联焰板堵塞的凹腔纵截面只有主涡,为稳定点火和火焰稳定提供条件;不同横截面的旋涡差别较大,离驻涡区前壁越远的截面涡心距越大,贴近前壁和后壁的截面均无旋涡;燃烧室入口速度对轴向中间截面的旋涡结构无影响,而前进口堵塞比对旋涡结构影响较大.

关 键 词:驻涡燃烧室  燃烧  驻涡区  涡系特点  数值模拟

Numerical Simulation on Characteristics of Vortex in Trapped Vortex Combustor
Authors:PENG Chun-mei  HE Xiao-min  JIN Yi
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:To investigate the distribution characteristics of the vortex in trapped vortex combustor cavity, FLUENT was used to perform numerical simulation on flow field of cavity with different blocking ratios of cavity front-inlet and different combustion inlet velocity. Pressure and steamline line of typical section was analyzed to research the characteristics of vortex in cavity. The result shows that the characteristics of vortex on different section are different, there only exist primary vortex on longitudinal section which mainstream was blockaded by shutter to help for the stability of ignition and flame stability. The differences of the vortex on different cross-sections are obvious. The distance between the vortex centers becomes larger as the distance to the front-wall increases. There is no vortex on cross-section which is close to front-wall and after-wall. The structure of the vortex on axial center section is not sensitive to combustor inlet velocity, but sensitive to blocking ratio of front-inlet.
Keywords:Trapped Vortex Combustor (TVC)  combustion  cavity  characteristics of vortex  numerical simulation
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