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基于半经验耦合的贫熄边界预测方法 被引量:2

Prediction method of lean blow-out limit based on a hybrid semi-empirical model
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摘要 提出了一种根据FV(flame volume)模型与燃烧室热态仿真相结合的贫油熄火边界耦合预测方法。利用两种不同构型五个不同方案燃烧室的贫熄试验数据对此方法进行验证,结果表明:对于直流型燃烧室与回流型燃烧室,FV模型中的经验常数K分别取1.35和0.55时,能够保证各方案燃烧室的贫油熄火边界预测精度均在±20%以内。相比于Lefebvre模型,此方法的计算精度更高、适用范围更广。 A new method for predicting the lean blow-out performance of the combustor was proposed by combining the FV model with the simulation of reacting flows.The data of lean blow-out experiment of 5 combustors(two of which are through-flow combustors and the rest are reverse-flow combustors)showed that,when the value of model constant K was1.35 to through-flow combustors,and 0.55 to reverse-flow combustors,the maximum uncertainties of the prediction method were less than±20%.And compared with the Lefebvre model,the method proposed is much more applicable and precise for combustors of various structures.
作者 陶焰明 肖为 江立军 TAO Yanming;XIAO Wei;JIANG Lijun(Combustor Research Department,Hunan Aviation Powerplant Research Institute,Aero Engine Corporation of China,Zhuzhou Hunan 412002,China)
出处 《航空动力学报》 EI CAS CSCD 北大核心 2019年第5期1111-1118,共8页 Journal of Aerospace Power
基金 中国航发自主创新专项资金(ZZCX-2017-018)
关键词 贫油熄火(LBO) 航空发动机燃烧室 半经验模型 火焰体积 油气比 lean blow-out(LBO) aero-engine combustor semi-empirical model flame volume fuel air ratio
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  • 1袁怡祥,林宇震,刘高恩.旋流杯燃烧室头部流场与喷雾对贫油熄火的影响[J].航空动力学报,2004,19(3):332-337. 被引量:34
  • 2张玉芳.燃烧室贫油熄火性能研究[D].北京:北京航空航天大学,2007.
  • 3Bahr D W. Technology for the design of high temperature rise combustors [ R ]. AIAA-85-1292,1985.
  • 4Lefebvre A H. Gas turbine combustion[ M ]. New York : McGraw- Hill, 1983.
  • 5Mellor A M. Design of modem turbine combustors[ M ]. London : Academic Press, 1990.
  • 6Ballal D R, Lefebvre A H. Weak extinction limits of turbulent flowing mixtures [ J]. Journal of Engineering for Power, 1979, 101:343 - 348.
  • 7Ballal D R, Lefebvre A H. Weak extinction limits of turbulent heterogeneous fuel/air mixtures [ J ]. Journal of Engineering for Power, 1980,102:416 - 421.
  • 8Lefebvre A H. Fuel effects on gas turbine combustion-ignition, stability, and combustion efficiency [ J ]. Transactions of the ASME,Journal of Engineering for Gas Turbines and Power,1985,107(1) :24 -37.
  • 9Ballal D R. Combustor stability & lean blowout[R]. AIAA-2004- 3526,2004.
  • 10Xie Fa, Huang Yong, Wang Fa, et al. Visualization of the lean blowout process in a model combustor with a swirl cup [ R ]. ASME-GT-2010-22534,2010.

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