Flow Field and Combustion Characterization of Premixed Gas Turbine Flames by Planar Laser Techniques

Author:

Stopper Ulrich1,Aigner Manfred1,Meier Wolfgang1,Sadanandan Rajesh1,Stöhr Michael1,Kim Ik Soo2

Affiliation:

1. German Aerospace Center, Institute of Combustion Technology, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany

2. Siemens Industrial Turbomachinery Ltd., P.O. Box 1, Waterside South, Lincoln LN5 7FD, UK

Abstract

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 Φ, and pressures up to p=6 bars. 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 chemiluminescence 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.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

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