journal6 ›› 2011, Vol. 32 ›› Issue (2): 65-70.

• 信息与工程 • 上一篇    下一篇

单、双环腔燃烧室燃烧性能的对比

  

  1. (1.北京航空航天大学热动力工程研究所,北京 100083;2.沈阳发动机设计所,辽宁  沈阳 110015)
  • 出版日期:2011-03-25 发布日期:2012-04-09

Combustion   Captibility  Comparison  of  Single Annular Combustor  and  Dual  Annular Combustor

  1. (1.School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing  100083,China;2.Shenyan  Aero-Engine  Design  Institute,Shenyang  110015,China)
  • Online:2011-03-25 Published:2012-04-09
  • About author:LI Feng(1966-),male,was born in Zixing County,Hunan Province,professor and director of doctor students at Beijing University of Aeronautics and Astronautics;research areas are combustion experiment and simulation.
  • Supported by:

    National  Natural Science Foundation of China(90716025;50476005)

摘要:保持单环腔主燃烧室的扩压器,外机匣最大直径尺寸以及喷口不变的前提下,将其火焰筒结构重新设计为并联式双环腔结构,设计了6种不同旋流器组合的双环腔结构燃烧室.采用相同的物理模型(包括湍流模型、辐射模型、喷雾模型及污染排放模型等),对单、双环腔主燃烧室分别进行全流程的三维计算.给出了燃烧室的总压恢复系数、燃烧效率、燃烧室出口温度分布系数、污染排放指标等燃烧室性能参数.对比分析了单、双环腔燃烧室的计算结果.结果表明,双环腔燃烧室置换单环腔燃烧室是可行的,该研究可为大飞机低污染大法动机的设计提供技术支持.

关键词: 燃烧室设计, 单环腔燃烧室, 双环腔燃烧室, 燃烧数值模拟

Abstract: In order to change a Single Annular Combustor(SAC) into a Dual Annular Combustor(DAC),the authors kept the diffuser,outer case and atomize of the SAC unchanged,redesigned the combustor from a single annular structure into a dual annular structure,and designed six different structure DAC.Taking the same physical models(including the turbulence,radiation,spray and emission models),simulations of three dimensional two-phase reacting turbulent flow in both the SAC and DAC were developed in the Fluent Code.The  total-pressure recovery coefficient,temperature distribution and exhaust emission levels were given.Finally,by comparing the simulation results,the feasibility of displacing the SAC into DAC structure  was certified.

Key words: combustors design;single annular combustor;dual annular combustor;combustion , simulation

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