58779 - Influence of Stator Hub Cavities on the Forced Response Behaviour of an Embedded Compressor Rotor 

This paper focusses on the impact of hub labyrinth seal leakage flows on the aeromechanical behavior of an embedded compressor rotor. End wall flows are critical in determining the performance of gas turbine engine compressors, particularly the hub leakage flows that can contribute to a significant reduction in performance due to the loss in efficiency induced by the leakage. While the current literature does contribute extensively to the understanding of the influence of this leakage flow on the performance, no attention has been given to its impact on the multi-row unsteady aerodynamic influence.   The authors of this paper have talked about the multi-row influence at various modes and operating condition using models without the hub cavities included []. The embedded compressor rotor utilized for this study is a part of a 3.5 stage subsonic rig located at the Zucrow lab, Purdue University. The current paper first addresses the steady aerodynamics of a multi-row compressor with hub cavities and talks in detail about the effect of cavities on the performance. Next the influence on the forcing function utilizing both 3-row(S1/R2/S2) and a 4-row(S1/R2/S2/R3) simulations at both the Peak efficiency (PE)and the High loading(HL) operating conditions is determined. To reduce the computational domain significantly the time transformation (TT) method was utilized within ANSYS CFX. The first part of the paper describes the multi-row influence of 2 neighboring stators having the same vane count, which excites the embedded rotor at the same frequency and the second part shows the influence of having physical waves reflecting from a rotating row downstream (R3).

                The results show the significance of modelling the stator hub cavities and the drastic improvement in the modal force prediction with the cavities included. However, the authors observed that the impact tends to be more significant when the computational domain is small, i.e. fewer rows are included. As the number of rows are increased the influence of hub cavities diminish. Some of the conclusions drawn from this study are: 1) The presence of hub cavities changes the angle of incidence thereby reducing flow separation at the hub. The influence of these propagate throughout the domain i.e. a change in the angle of incidence in the first stage has an effect even at a downstream row. 2) The modal force prediction improved by ~10% for the 3-row case and 1% for the 4-row case and the values moved closer to the experimental values in both cases. 3) The influence of hub cavities is more significant at torsional modes compared to higher order modes.

Keywords: Compressor, Forced response, multi-row, Mistuning, Stator hub cavities, CFD