Effect of Rub Grooves on Leakage and Windage Heating in Straight Through Labyrinth Seals

Abstract

Prediction of leakage flow and windage heating for labyrinth seals with honeycomb lands is critical in understanding gas turbine engine system performance and predicting its component life. There are several labyrinth seal configurations in use in gas turbines, and for each configuration, there are many geometric factors that can impact a seal's leakage and windage characteristics. One of the factors which has not been thoroughly investigated in previously published work is the presence of rubgrooves in the honeycomb land and its impact on seal performance. This paper describes the development of a numerical methodology aimed at studying this effect. Specifically, a threedimensional (3D) computational fluid dynamics (CFD) model is developed utilizing commercial finite volumebased software incorporating the renormalization group (RNG) kخµ turbulence model. Using this model, a broad parametric study is conducted by varying honeycomb cell size and radial clearance for a fourtooth straightthrough labyrinth seal with and without rubgrooves. The results show good agreement with available experimental data. They further indicate that presence of rubgrooves increases seal leakage and decreases windage heating. The absolute levels depend on the clearance and honeycomb cell size.