Abstract

The recirculation zone and the swirl flame behavior can be influenced by the burner exit shape, and few studies have been made into this structure. Large eddy simulation was carried out on 16 cases to distinguish critical geometry factors. The time series of the heat release rate were decomposed using seasonal-trend decomposition procedure to exclude the effect of short physical time. Dynamic mode decomposition (DMD) was performed to separate flame structures. The frequency characteristics extracted from the DMD modes were compared with those from the flame transfer functions. Results show that the flame cases can be categorized into three types, all of which are controlled by a specific geometric parameter. Except one type of flame, they show nonstationary behavior by the Kwiatkowski–Phillips–Schmidt–Shin test. The frequency bands corresponding to the coherent structures are identified. The flame transfer function indicates that the flame can respond to external excitation in the frequency range 100–300 Hz. The DMD modes capture the detailed flame structures. The higher frequency bands can be interpolated as the streamwise vortices and shedding vortices. The DMD modes, which correspond to the bands of flame transfer functions, can be estimated as streamwise vortices at the edges.

Highlights

  • Lean premixed combustion is one of the major trends for the development of a modern gas turbine combustor to achieve low NOx emissions

  • Contours of axial velocity (Figure 6) show that outer recirculation zone (ORZ) and center recirculation recirculation zone (CRZ) exist in all cases

  • The averaged static temperature at outlet in each was case compared with the mean value of 1640

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Summary

Introduction

Lean premixed combustion is one of the major trends for the development of a modern gas turbine combustor to achieve low NOx emissions. In this combustion scheme, the additional air and lower temperature at the flame front may cause instabilities during combustion. The additional air and lower temperature at the flame front may cause instabilities during combustion To solve this issue, additional recirculation zones must be formed in the combustor to effectively stabilize the flame under different operating conditions. The recirculation zones can provide local flow velocity to balance the turbulent flame speed. They provide long residence time and a radical pool for continuous burning. The flame can be stabilized in the designed location as a result of the above modifications

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