FLOW FIELD AND COMBUSTION CHARACTERIZATION OF PREMIXED GAS TURBINE FLAMES BY PLANAR LASER TECHNIQUES

被引:0
|
作者
Stopper, Ulrich [1 ]
Aigner, Manfred [1 ]
Meier, Wolfgang [1 ]
Sadanandan, Rajesh [1 ]
Stoehr, Michael [1 ]
Kim, Ik Soo
机构
[1] German Aerosp Ctr, Inst Combust Technol, D-70569 Stuttgart, Germany
来源
PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 3, PTS A AND B | 2008年
关键词
lean premixed combustion; swirl flow; gas turbine combustor; high pressure; NOx reduction; OH* chemiluminescence; laser diagnostics; OH PLIF; PIV; reaction zone; heat release; turbulent flow field; vortex core; validation data;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Lean premixed natural gas/air,flames produced by an industrial gas turbine burner were analyzed using laser diagnostic methods. For this purpose, the burner was equipped with an optical combustion chamber and operated with preheated air at various thermal powers P, equivalence ratios (P, and pressures up to p=6 bar For the visualization of the flame emissions OH* chemiluminescence imaging was applied. Absolute flow velocities were measured using particle image velocimetry (PIV), and the reaction zones as well as regions of burnt gas were characterized by planar laser induced fluorescence (PLIF) of OH. Using these techniques, the combustion behavior was characterized in detail. The mean flow field could be divided into different regimes: the inflow, a central and an outer recirculation zone, and the outgoing exhaust flow Single-shot PIV images demonstrated that the instantaneous flow field was composed of small and medium sized vortices, mainly located along the shear layers. The chemi-luminescence images reflected the regions of heat release. From the PLIF images it was seen that the primary reactions are located in the shear layers between the inflow and the recirculation zones and that the appearance of the reaction zones changed with flame parameters.
引用
收藏
页码:419 / 429
页数:11
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