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dc.contributor.authorPhan, H. M.
dc.contributor.authorPekris, M. J.
dc.contributor.authorChew, J. W.
dc.date.accessioned2024-04-24T22:27:34Z
dc.date.available2024-04-24T22:27:34Z
dc.date.copyright2/8/2024 12:00:00 AM
dc.date.issued2024
dc.identifier.issn0742-4795
dc.identifier.othergtp_146_08_081010.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295256
dc.description.abstractBrush seals offer a superior sealing effectiveness compared to labyrinth seals. However, widespread use of brush seals is constrained by deleterious behaviors such as pressure-stiffening and hysteresis. For the latter, the bristles bend during the shaft incursion process and do not fully recover during the shaft retraction process. An opening gap is created, which increases seal leakage unless the pressure load drops to a certain level. In this work, analytical and numerical models based on a single bristle are proposed to capture the seal's response to shaft displacement with and without pressure loading. The models are validated using static stiffness tests at an unpressurized condition from literature. The main results show that modeling of the backing ring friction is essential to capture the bristle hang-up behavior. Shaft friction dominates at unpressurized conditions, while backing ring friction dominates at high pressure loading. An expression for shaft hang-up displacement has been derived. A sensitivity study shows that seals with shallow lay angle, short bristle length, and large bristle diameter are less prone to hang-up problems. The models developed in the present framework have been shown to qualitatively capture the pressure stiffening, hysteresis, bristle hang-up, and shaft rotation effects.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleInsights Into Frictional Brush Seal Hysteresis
dc.typeJournal Paper
dc.journal.volume146
dc.journal.issue8
dc.journal.titleJournal of Engineering for Gas Turbines and Power
dc.identifier.doi10.1115/1.4064151
dc.journal.fristpage81010-1
dc.journal.lastpage81010-12
dc.page12
dc.treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 008
dc.contenttypeFulltext


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