In this paper, a hybrid brush pocket damper seal is studied
theoretically using computational fluid dynamics. In the hybrid
sealing arrangement, the brush seal element with cold clearance
is placed downstream of a 4-bladed, 8-pocket, fully partitioned
pocket damper seal. The new seal geometry is derived based on
designs of short brush-labyrinth seals studied in previous works.
Transient CFD simulations coupled with the multi-frequency rotor
excitation method are performed to determine frequencydependent
stiffness and damping coefficients of pocket damper
seals. A moving mesh technique is applied to model the shaft
motion on a predefined whirling orbit. The rotordynamic coeffi-
cients are calculated from impedances obtained in frequency domain.
The pocket damper seal CFD model is validated against
available experimental and numerical results found in the literature.
Bristle pack in the brush seal CFD model is described as
porous medium. The applied brush seal model is validated using
the measurements obtained in previous works from two test
rigs. Predicted leakage characteristics as well as stiffness and
damping coefficients of the hybrid brush pocket damper seal are
presented for different operating conditions. In this case, the rotordynamic
coefficients are calculated using a single-frequency
transient simulation. By adding the brush seal, direct stiffness is predicted to be significantly decreased while effective damping
shows a more moderate or no reduction depending on excitation
frequency. Effective clearance results indicate more than halved
leakage compared to the case without brush seal.
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In this paper, a hybrid brush pocket damper seal is studied
theoretically using computational fluid dynamics. In the hybrid
sealing arrangement, the brush seal element with cold clearance
is placed downstream of a 4-bladed, 8-pocket, fully partitioned
pocket damper seal. The new seal geometry is derived based on
designs of short brush-labyrinth seals studied in previous works.
Transient CFD simulations coupled with the multi-frequency rotor
excitation method are performed to determine fre...
»