Abstract

A production gas turbine combustor swirl cup and a 3x-scale model, both featuring co-axial, counter-swirling air streams are characterized at atmospheric pressure and in the absence of reaction. Spatially-resolved measurements of continuous phase (gas in the presence of spray) and droplet size and velocity are acquired downstream of the production and 3x-scale swirl cups by using two-component phase Doppler interferometry. The effect of scale on the behavior of the continuous phase and droplets is investigated by comparing the continuous phase velocity and droplet size and velocity at geometrically analogous positions. The continuous phase flow field scales well at the exit of the swirl cup. Farther downstream, differences occur which are due to disparity in entrainment. The droplet velocities scale reasonably well, but the sizes show some differences. However, the difference in size is less significant than it is between the two atomizers in the absence of the swirl cup assemblies.

Highlights

  • A production gas turbine combustor swirl cup and a 3x-scale model, both featuring co-axial, counter-swirling air streams are characterized at a tmospheric pressure and in the absence of reaction

  • The effect of scale on the behavior of the continuous phase and droplets is investigated by comparing the continuous phase velocity and droplet size and velocity at geometrically analogous positions

  • The continuous phase flow field scales weU at the exit of the swirl cup

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Summary

Introduction

In this swirl cup assembly, fuel is injected by a simplex atomizer mounted in the center of the swirl cup. Due to the complexity of the co-axial, counter-swirling air flows and the lack of adequate advanced diagnostics, few studies have been conducted on gas-liquid two-phase flow in the presence of such flows. The droplet size and velocity distributions are obtained downstream of a production GE CFM56 engine combustor swirl cup upon which the 3x-scale model is based. A 6.35 mm polycarbonate honeycomb (101.6 mm thick) was placed about 50 mm above the top of the swirl cup in both cases to provide a uniform velocity profiles at the entrance plane to the swirlers

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