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基于分层和分级燃烧机理的低污染燃烧室设计和排放性能预估

李锋 郭瑞卿 高贤智 吕富国 王云雷 尚守堂

李锋, 郭瑞卿, 高贤智, 吕富国, 王云雷, 尚守堂. 基于分层和分级燃烧机理的低污染燃烧室设计和排放性能预估[J]. 航空动力学报, 2014, 29(12): 2795-2800. doi: 10.13224/j.cnki.jasp.2014.12.002
引用本文: 李锋, 郭瑞卿, 高贤智, 吕富国, 王云雷, 尚守堂. 基于分层和分级燃烧机理的低污染燃烧室设计和排放性能预估[J]. 航空动力学报, 2014, 29(12): 2795-2800. doi: 10.13224/j.cnki.jasp.2014.12.002
LI Feng, GUO Rui-qing, GAO Xian-zhi, LÜ Fu-guo, WANG Yun-lei, SHANG Shou-tang. Low pollution combustor design and emission performance prediction based on stratified and staged combustion mechanism[J]. Journal of Aerospace Power, 2014, 29(12): 2795-2800. doi: 10.13224/j.cnki.jasp.2014.12.002
Citation: LI Feng, GUO Rui-qing, GAO Xian-zhi, LÜ Fu-guo, WANG Yun-lei, SHANG Shou-tang. Low pollution combustor design and emission performance prediction based on stratified and staged combustion mechanism[J]. Journal of Aerospace Power, 2014, 29(12): 2795-2800. doi: 10.13224/j.cnki.jasp.2014.12.002

基于分层和分级燃烧机理的低污染燃烧室设计和排放性能预估

doi: 10.13224/j.cnki.jasp.2014.12.002
基金项目: 

航天支撑基金(13131001)

国家自然科学基金(91441108)

航天创新重点基金(CASC03)

详细信息
    作者简介:

    李锋(1966-), 男, 湖南资兴人, 教授、博士生导师, 博士后, 主要从事燃烧、流动控制及隐身的研究.

  • 中图分类号: V231.1

Low pollution combustor design and emission performance prediction based on stratified and staged combustion mechanism

  • 摘要: 保持扩压器尺寸、外机匣最大直径以及燃烧室出口尺寸不变,将燃烧室分别设计为单环腔燃烧室(SAC)、双环腔燃烧室(DAC)、双环预混旋流(TAPS)燃烧室、中心分级燃烧室(CSC)和三旋流燃烧室(TSC)5种燃烧室结构,保持湍流、喷雾、燃烧、辐射及排放数理模型不变,对5种燃烧室进行三维数值模拟.对比研究了5种燃烧室的污染排放性能.结果表明:采用分级燃烧的DAC慢车状态下CO排放量最低,采用DAC在慢车状态下的CO排放量比SAC降低了近62%.采用分层燃烧的TAPS燃烧室的NOx排放量最低,采用TAPS的NOx排放量比SAC降低了近43.5%.

     

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出版历程
  • 收稿日期:  2013-12-08
  • 刊出日期:  2014-12-28

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