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Influence of Leak Path Friction on Labyrinth Seal Inlet Swirl
Labyrinth seals in various kinds of rotating machinery often generate driving force components that may increase the unstable vibration of the rotor. The evaluation of labyrinth seal forces has been documented by CFD analysis but the leak path geometry influence on the resulting entry and reverse pu...
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Published in: | Tribology transactions 2009-03, Vol.52 (2), p.139-145 |
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creator | Kirk, R. G. Guo, Z. |
description | Labyrinth seals in various kinds of rotating machinery often generate driving force components that may increase the unstable vibration of the rotor. The evaluation of labyrinth seal forces has been documented by CFD analysis but the leak path geometry influence on the resulting entry and reverse pumping flow prior to the labyrinth seal geometry has only recently been studied in detail. The labyrinth seal driving forces are known to increase with an increase of the inlet swirl velocity ratio. In a previous work, a commercial CFD program was used to simulate leak path and labyrinth seal flows of various centrifugal compressor eye seal leak flow geometries. For each case, 3D models with an eccentric rotor were solved to obtain the leakage flow, velocity vector, chamber pressure, and the average chamber swirl entering the seal. The current article will present the bulk flow analysis predicted entry swirl ratio for the same geometries and sealing conditions. The influence of the effective disk friction will be considered in the calculation of the bulk flow results by using modified turbulence factors. The CFD simulation showed that the inlet geometry and the resultant reverse pumping flow in the entry channel can have a significant influence on the calculated chamber average swirl velocity ratio. Generally, the bulk flow analysis gives a pessimistic estimate of the swirl velocities as compared to the CFD calculations. |
doi_str_mv | 10.1080/10402000802105430 |
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G. ; Guo, Z.</creator><creatorcontrib>Kirk, R. G. ; Guo, Z.</creatorcontrib><description>Labyrinth seals in various kinds of rotating machinery often generate driving force components that may increase the unstable vibration of the rotor. The evaluation of labyrinth seal forces has been documented by CFD analysis but the leak path geometry influence on the resulting entry and reverse pumping flow prior to the labyrinth seal geometry has only recently been studied in detail. The labyrinth seal driving forces are known to increase with an increase of the inlet swirl velocity ratio. In a previous work, a commercial CFD program was used to simulate leak path and labyrinth seal flows of various centrifugal compressor eye seal leak flow geometries. For each case, 3D models with an eccentric rotor were solved to obtain the leakage flow, velocity vector, chamber pressure, and the average chamber swirl entering the seal. The current article will present the bulk flow analysis predicted entry swirl ratio for the same geometries and sealing conditions. The influence of the effective disk friction will be considered in the calculation of the bulk flow results by using modified turbulence factors. The CFD simulation showed that the inlet geometry and the resultant reverse pumping flow in the entry channel can have a significant influence on the calculated chamber average swirl velocity ratio. Generally, the bulk flow analysis gives a pessimistic estimate of the swirl velocities as compared to the CFD calculations.</description><identifier>ISSN: 1040-2004</identifier><identifier>EISSN: 1547-397X</identifier><identifier>DOI: 10.1080/10402000802105430</identifier><identifier>CODEN: TRTRE4</identifier><language>eng</language><publisher>Philadelphia, PA: Taylor & Francis Group</publisher><subject>Applied sciences ; Drives ; Estimates ; Exact sciences and technology ; Friction, wear, lubrication ; Geometry ; Labyrinth ; Leakage ; Machine components ; Machinery ; Mechanical engineering. Machine design ; Rotordynamics ; Seals ; Seals and gaskets ; Shafts, couplings, clutches, brakes ; Simulation ; Stability ; Tribology ; Velocity</subject><ispartof>Tribology transactions, 2009-03, Vol.52 (2), p.139-145</ispartof><rights>Copyright Taylor & Francis Group, LLC 2009</rights><rights>2009 INIST-CNRS</rights><rights>Copyright Taylor & Francis Inc. Mar 2009</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c434t-1e8eab59d14dff924ad2b4ab9da3fb19dc04eea16cfdb3194fa3cd1db70c3a793</citedby><cites>FETCH-LOGICAL-c434t-1e8eab59d14dff924ad2b4ab9da3fb19dc04eea16cfdb3194fa3cd1db70c3a793</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=21228122$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Kirk, R. G.</creatorcontrib><creatorcontrib>Guo, Z.</creatorcontrib><title>Influence of Leak Path Friction on Labyrinth Seal Inlet Swirl</title><title>Tribology transactions</title><description>Labyrinth seals in various kinds of rotating machinery often generate driving force components that may increase the unstable vibration of the rotor. The evaluation of labyrinth seal forces has been documented by CFD analysis but the leak path geometry influence on the resulting entry and reverse pumping flow prior to the labyrinth seal geometry has only recently been studied in detail. The labyrinth seal driving forces are known to increase with an increase of the inlet swirl velocity ratio. In a previous work, a commercial CFD program was used to simulate leak path and labyrinth seal flows of various centrifugal compressor eye seal leak flow geometries. For each case, 3D models with an eccentric rotor were solved to obtain the leakage flow, velocity vector, chamber pressure, and the average chamber swirl entering the seal. The current article will present the bulk flow analysis predicted entry swirl ratio for the same geometries and sealing conditions. The influence of the effective disk friction will be considered in the calculation of the bulk flow results by using modified turbulence factors. The CFD simulation showed that the inlet geometry and the resultant reverse pumping flow in the entry channel can have a significant influence on the calculated chamber average swirl velocity ratio. Generally, the bulk flow analysis gives a pessimistic estimate of the swirl velocities as compared to the CFD calculations.</description><subject>Applied sciences</subject><subject>Drives</subject><subject>Estimates</subject><subject>Exact sciences and technology</subject><subject>Friction, wear, lubrication</subject><subject>Geometry</subject><subject>Labyrinth</subject><subject>Leakage</subject><subject>Machine components</subject><subject>Machinery</subject><subject>Mechanical engineering. Machine design</subject><subject>Rotordynamics</subject><subject>Seals</subject><subject>Seals and gaskets</subject><subject>Shafts, couplings, clutches, brakes</subject><subject>Simulation</subject><subject>Stability</subject><subject>Tribology</subject><subject>Velocity</subject><issn>1040-2004</issn><issn>1547-397X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2009</creationdate><recordtype>article</recordtype><recordid>eNqFkE1LAzEQhhdRsFZ_gLdF0NtqJsl2d0EPUvwoFBRU8BZm84Fb00STLbX_3kjVgyJCQobJ87wMk2X7QI6B1OQECCeUkFRSICVnZCMbQMmrgjXV42aq03-RAL6d7cQ4IwRKADbIzibO2IV2Uufe5FONz_kt9k_5Zehk33mXpzPFdhU6l7p3Gm0-cVb3-d2yC3Y32zJoo977fIfZw-XF_fi6mN5cTcbn00JyxvsCdK2xLRsFXBnTUI6KthzbRiEzLTRKEq41wkga1TJouEEmFai2IpJh1bBhdrTOfQn-daFjL-ZdlNpadNovomCsqmsGLIEHP8CZXwSXZhOUlmw0GpUfabCGZPAxBm3ES-jmGFYCiPjYpvi1zeQcfgZjlGhNQCe7-C1SoLRON3HVmuuc8WGOSx-sEj2urA9f0q900b_1yTz912R_D_gOxcqYRw</recordid><startdate>200903</startdate><enddate>200903</enddate><creator>Kirk, R. G.</creator><creator>Guo, Z.</creator><general>Taylor & Francis Group</general><general>Taylor & Francis</general><general>Taylor & Francis Inc</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>7U5</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>L7M</scope></search><sort><creationdate>200903</creationdate><title>Influence of Leak Path Friction on Labyrinth Seal Inlet Swirl</title><author>Kirk, R. G. ; Guo, Z.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c434t-1e8eab59d14dff924ad2b4ab9da3fb19dc04eea16cfdb3194fa3cd1db70c3a793</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2009</creationdate><topic>Applied sciences</topic><topic>Drives</topic><topic>Estimates</topic><topic>Exact sciences and technology</topic><topic>Friction, wear, lubrication</topic><topic>Geometry</topic><topic>Labyrinth</topic><topic>Leakage</topic><topic>Machine components</topic><topic>Machinery</topic><topic>Mechanical engineering. Machine design</topic><topic>Rotordynamics</topic><topic>Seals</topic><topic>Seals and gaskets</topic><topic>Shafts, couplings, clutches, brakes</topic><topic>Simulation</topic><topic>Stability</topic><topic>Tribology</topic><topic>Velocity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kirk, R. G.</creatorcontrib><creatorcontrib>Guo, Z.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Tribology transactions</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kirk, R. G.</au><au>Guo, Z.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Influence of Leak Path Friction on Labyrinth Seal Inlet Swirl</atitle><jtitle>Tribology transactions</jtitle><date>2009-03</date><risdate>2009</risdate><volume>52</volume><issue>2</issue><spage>139</spage><epage>145</epage><pages>139-145</pages><issn>1040-2004</issn><eissn>1547-397X</eissn><coden>TRTRE4</coden><abstract>Labyrinth seals in various kinds of rotating machinery often generate driving force components that may increase the unstable vibration of the rotor. The evaluation of labyrinth seal forces has been documented by CFD analysis but the leak path geometry influence on the resulting entry and reverse pumping flow prior to the labyrinth seal geometry has only recently been studied in detail. The labyrinth seal driving forces are known to increase with an increase of the inlet swirl velocity ratio. In a previous work, a commercial CFD program was used to simulate leak path and labyrinth seal flows of various centrifugal compressor eye seal leak flow geometries. For each case, 3D models with an eccentric rotor were solved to obtain the leakage flow, velocity vector, chamber pressure, and the average chamber swirl entering the seal. The current article will present the bulk flow analysis predicted entry swirl ratio for the same geometries and sealing conditions. The influence of the effective disk friction will be considered in the calculation of the bulk flow results by using modified turbulence factors. The CFD simulation showed that the inlet geometry and the resultant reverse pumping flow in the entry channel can have a significant influence on the calculated chamber average swirl velocity ratio. Generally, the bulk flow analysis gives a pessimistic estimate of the swirl velocities as compared to the CFD calculations.</abstract><cop>Philadelphia, PA</cop><pub>Taylor & Francis Group</pub><doi>10.1080/10402000802105430</doi><tpages>7</tpages></addata></record> |
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source | Taylor and Francis:Jisc Collections:Taylor and Francis Read and Publish Agreement 2024-2025:Science and Technology Collection (Reading list) |
subjects | Applied sciences Drives Estimates Exact sciences and technology Friction, wear, lubrication Geometry Labyrinth Leakage Machine components Machinery Mechanical engineering. Machine design Rotordynamics Seals Seals and gaskets Shafts, couplings, clutches, brakes Simulation Stability Tribology Velocity |
title | Influence of Leak Path Friction on Labyrinth Seal Inlet Swirl |
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