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 coefficients 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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ASME Turbo Expo 2015: Turbine Technical Conference and Exposition
June 15–19, 2015
Montreal, Quebec, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5676-5
PROCEEDINGS PAPER
Segmentation Effects on Brush Seal Leakage and Rotordynamic Coefficients
Alexander O. Pugachev,
Alexander O. Pugachev
Technische Universitaet Muenchen, Garching, Germany
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Manuel Gaszner,
Manuel Gaszner
Technische Universitaet Muenchen, Garching, Germany
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Paul Cooper
Paul Cooper
ALSTOM, Rugby, UK
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Alexander O. Pugachev
Technische Universitaet Muenchen, Garching, Germany
Manuel Gaszner
Technische Universitaet Muenchen, Garching, Germany
Christos Georgakis
ALSTOM, Rugby, UK
Paul Cooper
ALSTOM, Rugby, UK
Paper No:
GT2015-42332, V07AT31A004; 12 pages
Published Online:
August 12, 2015
Citation
Pugachev, AO, Gaszner, M, Georgakis, C, & Cooper, P. "Segmentation Effects on Brush Seal Leakage and Rotordynamic Coefficients." Proceedings of the ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. Volume 7A: Structures and Dynamics. Montreal, Quebec, Canada. June 15–19, 2015. V07AT31A004. ASME. https://doi.org/10.1115/GT2015-42332
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