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dc.contributor.authorBird, Joshua
dc.contributor.authorKeogh, Patrick S.
dc.contributor.authorSangan, Carl M.
dc.contributor.authorBowsher, Aaron A.
dc.contributor.authorCrudgington, Peter F.
dc.contributor.authorScobie, James A.
dc.date.accessioned2024-04-24T22:24:26Z
dc.date.available2024-04-24T22:24:26Z
dc.date.copyright11/21/2023 12:00:00 AM
dc.date.issued2023
dc.identifier.issn0742-4795
dc.identifier.othergtp_146_01_011017.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295161
dc.description.abstractShaft seals control the leakage of fluid between areas of high pressure and low pressure around rotating components inside turbomachinery. Static seals are often subject to damaging rubs with the shaft, caused by assembly misalignments and rotordynamic vibrations during operation. Adaptive seals aim to reduce leakage flows whilst minimizing wear. The film riding pressure actuated leaf seal (FRPALS) is one such design which utilizes a large installation clearance and is blown down toward the shaft under pressure. This paper presents a numerical model which can be used in the design and development of adaptive shaft seals, validated by experimental data from the literature. The model uses a modified version of the Reynolds equation to predict the dynamic, frequency-dependent stiffness and damping coefficients of the fluid film. The dynamic coefficients have been solved for different operational clearances and pressure differences to generate coefficient maps. These maps have been incorporated into a blow down model with compliant mechanical leaves to predict the transient translational and angular displacement paths of the FRPALS when subject to an increasing pressure drop. The blow down model has been compared against experimental measurements collected from a specially designed test facility for the characterization of shaft seal performance. Eddy current probes were used to measure the displacement paths of the FRPALS with the experimental values showing that the model can accurately predict the dynamic movement of the seal when subject to a pressure difference.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleDynamic Characterization of an Adaptive Film-Riding Seal
dc.typeJournal Paper
dc.journal.volume146
dc.journal.issue1
dc.journal.titleJournal of Engineering for Gas Turbines and Power
dc.identifier.doi10.1115/1.4063549
dc.journal.fristpage11017-1
dc.journal.lastpage11017-12
dc.page12
dc.treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 001
dc.contenttypeFulltext


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