Experimental study on NOemission correlation of fuel staged combustion in a LPP combustor at high pressure based on NO-chemiluminescence

被引:0
作者
Zhichao WANG [1 ]
Yuzhen LIN [1 ]
Jianchen WANG [1 ]
Chi ZHANG [1 ]
Zhijun PENG [2 ]
机构
[1] National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,Collaborative Innovation Center for Advanced Aero-Engine,School of Energy and Power Engineering,Beihang University
[2] Creative Arts,Technologies and Science,University of Bedfordshire
关键词
Combustors; Lean staged combustion; Low emissions; NOx correlation; Optical diagnosis;
D O I
暂无
中图分类号
V231.2 [燃烧理论];
学科分类号
082502 ;
摘要
Experimental investigations on NOx emissions of a single-cup,Lean Premixed Prevaporized (LPP),module combustor were carried out at elevated inlet temperature and pressure up to810 K and 2.0 MPa,close to the real operating conditions of aero-engine combustors.This LPP combustor adopts centrally staged fuel injections which could produce separated stratified swirling spray flame.In the NOx emissions measurements,the ranges of dome equivalence ratio and fuel stage ratio were from 0.55 to 0.58 and 8%to 24%,respectively.The optical diagnosis on separated stratified swirling spray flame were carried out with fuel stage ratio changing from 15%to 30%.Therefore,NO*and OH*chemiluminescence images were obtained.The results show that NOx emissions increase with the increase of the fuel stage ratio.And from the chemiluminescence images,the main flame and pilot flame are found weakly coupled.The pilot flame plays a significant role in NOx emission production because of its higher adiabatic flame temperature.Based on the results of chemiluminescence optical tests,a new NOx emission prediction model is proposed based on the Lefebvre's single flame model The estimate of local equivalence ratio of the pilot stage's nonpremixed flame is modified considering the characteristics of spray combustion,and a"PLUS"emission prediction model suitable for separated stratified swirling spray flame is obtained.Compared to the experimental data,the"PLUS"model exhibits a good prediction in a range of±13%of deviation.
引用
收藏
页码:550 / 560
页数:11
相关论文
共 17 条
[1]  
Large-eddy simulation and linear acoustic modeling of entropy mode oscillations in a model combustor with coolant injection[J]. Man ZHANG,An LIANG.Chinese Journal of Aeronautics. 2018(08)
[2]  
Review of modern low emissions combustion technologies for aero gas turbine engines[J] . Yize Liu,Xiaoxiao Sun,Vishal Sethi,Devaiah Nalianda,Yi-Guang Li,Lu Wang.Progress in Aerospace Sciences . 2017
[3]  
Emission characteristics of a model combustor for aero gas turbine application[J] . Li Lin,Lin Yuzhen,Fu Zhenbo,Zhang chi.Experimental Thermal and Fluid Science . 2015
[4]  
The role of separation of scales in the description of spray combustion[J] . Antonio L. Sánchez,Javier Urzay,Amable Li?án.Proceedings of the Combustion Institute . 2015 (2)
[5]  
Experimental study of NO x correlation for fuel staged combustion using lab-scale gas turbine combustor at high pressure[J] . Dong-Sik Han,Gyu-Bo Kim,Han-Suk Kim,Chung-Hwan Jeon.Experimental Thermal and Fluid Science . 2014
[6]  
Experimental and numerical studies of a lean-burn internally-staged combustor[J] . Zhenbo Fu,Yuzhen Lin,Lin Li,Chi Zhang.Chinese Journal of Aeronautics . 2013
[7]  
Simultaneous visualization of OH, CH, CH 2 O and toluene PLIF in a methane jet flame with varying degrees of turbulence[J] . Johan Sj?holm,Joakim Rosell,Bo Li,Mattias Richter,Zhongshan Li,Xue-Song Bai,Marcus Aldén.Proceedings of the Combustion Institute . 2013 (1)
[8]  
CFD Study of NO x Emissions in a Model Commercial Aircraft Engine Combustor[J] . Man ZHANG,Zhenbo FU,Yuzhen LIN,Jibao LI.Chinese Journal of Aeronautics . 2012 (6)
[9]  
Lean-limit combustion instabilities of a lean premixed prevaporized gas turbine combustor[J] . Sulabh K. Dhanuka,Jacob E. Temme,James F. Driscoll.Proceedings of the Combustion Institute . 2010 (2)
[10]  
Vortex-shedding and mixing layer effects on periodic flashback in a lean premixed prevaporized gas turbine combustor[J] . Sulabh K. Dhanuka,Jacob E. Temme,James F. Driscoll,Hukam C. Mongia.Proceedings of the Combustion Institute . 2009 (2)