Abstract

To reduce gas leakage, shape optimization of a straight labyrinth seal was carried out. The six design parameters included seal clearance, fin width, fin height, fin pitch, fin backward, and forward expansion angle. The CFD (Computational Fluid Dynamics) model was solved to generate the training and testing samples for the surrogate model, which was established by the least square support vector machine. A kind of chaotic optimization algorithm was used to determine the optimal design parameters of the labyrinth seal. As seal clearance, fin width, fin height, fin pitch, fin backward and forward expansion angles are 0.2 mm, 0.1 mm, 7 mm, 9 mm, 0°, and 15°, the discharge coefficient can reach its minimum value in the design space. The chaotic optimization algorithm coupled with least square support vector machine is a promising scheme for labyrinth seal optimization.

Highlights

  • Aerospace 2021, 8, 92. https://With the increase of operation pressure, leakage in gas turbines has attracted more and more attention

  • Their experimental results showed that increasing the seal clearance, fin width, and fin height all lead to an increase of discharge coefficient, while adding the fin pitch causes the decrease of the discharge coefficient

  • The effects of fin width and seal clearance on the discharge coefficient are shown in Adding of sealfin clearance to seal the decrease of the velocity, which coefficient lowered the

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Summary

Introduction

Aerospace 2021, 8, 92. https://With the increase of operation pressure, leakage in gas turbines has attracted more and more attention. The main advantages of labyrinth seals are high flow resistance, structural reliability, and simplicity. The influence of fin-shaped parameters on leakage were studied by Du et al [4] in straight labyrinth seals. Their experimental results showed that increasing the seal clearance, fin width, and fin height all lead to an increase of discharge coefficient, while adding the fin pitch causes the decrease of the discharge coefficient. The discharge coefficient relies on the number of seal fins, fin height, fin pitch, pressure ratio, seal clearance, step shift, honeycomb cell diameter, fin width, groove shift, step height, and groove width.

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