This paper studies the effect of brush seal segmentation on
the seal performance characteristics. A brush-labyrinth sealing
configuration arranged of one brush seal downstream and two
labyrinth fins upstream is studied experimentally and theoretically.
The studied brush seal is of welded design installed with
zero cold radial clearance. The brush seal front and back rings
as well as the bristle pack are segmented radially in a single
plane using the electrical discharge machining technique. The
segmentation procedure results in loss of bristles at the site of
the cuts altering the leakage flow structure in the seal and its
performance characteristics. Two test rigs are used to obtain
leakage, as well as rotordynamic stiffness and damping coeffi-
cients of the seal at different pressure ratios. The CFD-based
model is used to predict the seal performance and to study in detail
local changes in the flow field due to the segmentation. A
back-to-back comparison of the performance of non-segmented
and segmented brush seals, as well as baseline labyrinth seal is
provided. The obtained results demonstrate that the segmentation
in general negatively affects the performance of the studied
brush-labyrinth sealing configuration. However, the segmented
brush seal shows increased direct damping coefficients.
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