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Brush Seal Leakage Performance With Gaseous Working Fluids at Static and Low Rotor Speed Conditions
The leakage performance of a brush seal with gaseous working fluids at static and low rotor speed conditions was investigated. This report includes the leakage results for air, helium, and carbon dioxide at several bristle/rotor interferences. In addition, the effects of packing a lubricant into the...
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Published in: | Journal of engineering for gas turbines and power 1993-04, Vol.115 (2), p.397-403 |
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container_title | Journal of engineering for gas turbines and power |
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creator | Carlile, J. A Hendricks, R. C Yoder, D. A |
description | The leakage performance of a brush seal with gaseous working fluids at static and low rotor speed conditions was investigated. This report includes the leakage results for air, helium, and carbon dioxide at several bristle/rotor interferences. In addition, the effects of packing a lubricant into the bristles and also of reversing the pressure drop across the seal were investigated. Results were compared to that of an annular seal at similar operating conditions. In order to generalize the results, they were correlated using corresponding state theory. The brush seal tested had a bore diameter of 3.792 cm (1.4930 in.), a fence height of 0.0635 cm (0.025 in.), and 1800 bristles/cm-circumference (4500 bristles/in.-circumference). Various bristle/rotor radial interferences were achieved by using a tapered rotor. The brush seal reduced the leakage in comparison with the annular seal, up to 9.5 times. Reversing the pressure drop across the brush seal produced leakage rates approximately the same as that of the annular seal. Addition of a lubricant reduced the leakage by 2.5 times when compared to a nonlubricated brush seal. The air and carbon dioxide data were successfully correlated using the corresponding state theory. However, the helium data followed a different curve from the air and carbon dioxide data. |
doi_str_mv | 10.1115/1.2906722 |
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A ; Hendricks, R. C ; Yoder, D. A</creator><creatorcontrib>Carlile, J. A ; Hendricks, R. C ; Yoder, D. A</creatorcontrib><description>The leakage performance of a brush seal with gaseous working fluids at static and low rotor speed conditions was investigated. This report includes the leakage results for air, helium, and carbon dioxide at several bristle/rotor interferences. In addition, the effects of packing a lubricant into the bristles and also of reversing the pressure drop across the seal were investigated. Results were compared to that of an annular seal at similar operating conditions. In order to generalize the results, they were correlated using corresponding state theory. The brush seal tested had a bore diameter of 3.792 cm (1.4930 in.), a fence height of 0.0635 cm (0.025 in.), and 1800 bristles/cm-circumference (4500 bristles/in.-circumference). Various bristle/rotor radial interferences were achieved by using a tapered rotor. The brush seal reduced the leakage in comparison with the annular seal, up to 9.5 times. Reversing the pressure drop across the brush seal produced leakage rates approximately the same as that of the annular seal. Addition of a lubricant reduced the leakage by 2.5 times when compared to a nonlubricated brush seal. The air and carbon dioxide data were successfully correlated using the corresponding state theory. However, the helium data followed a different curve from the air and carbon dioxide data.</description><identifier>ISSN: 0742-4795</identifier><identifier>EISSN: 1528-8919</identifier><identifier>DOI: 10.1115/1.2906722</identifier><identifier>CODEN: JETPEZ</identifier><language>eng</language><publisher>New York, NY: ASME</publisher><subject>20 FOSSIL-FUELED POWER PLANTS ; 200104 - Fossil-Fueled Power Plants- Components ; 330103 - Internal Combustion Engines- Turbine ; ADVANCED PROPULSION SYSTEMS ; AIR ; Applied sciences ; CARBON COMPOUNDS ; CARBON DIOXIDE ; CARBON OXIDES ; CHALCOGENIDES ; DATA ; ELEMENTS ; Energy ; Energy. Thermal use of fuels ; Engines and turbines ; Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc ; Exact sciences and technology ; EXPERIMENTAL DATA ; FLUID FLOW ; FLUIDS ; Gas engines ; Gas turbines ; GASES ; HELIUM ; INFORMATION ; Leakage (fluid) ; LUBRICANTS ; NONMETALS ; NUMERICAL DATA ; OXIDES ; OXYGEN COMPOUNDS ; PERFORMANCE TESTING ; Pressure measurement ; RARE GASES ; ROTORS ; SEALS ; SUBSONIC FLOW ; TESTING ; Thermal effects</subject><ispartof>Journal of engineering for gas turbines and power, 1993-04, Vol.115 (2), p.397-403</ispartof><rights>1993 INIST-CNRS</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a370t-e38a319f403212b282563843208b7fc248e4a9d358ebd854f6822db9cc3ca68a3</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,309,310,314,776,780,785,786,881,23911,23912,25120,27903,27904,38498</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=4875599$$DView record in Pascal Francis$$Hfree_for_read</backlink><backlink>$$Uhttps://www.osti.gov/biblio/6504593$$D View this record in Osti.gov$$Hfree_for_read</backlink></links><search><creatorcontrib>Carlile, J. A</creatorcontrib><creatorcontrib>Hendricks, R. C</creatorcontrib><creatorcontrib>Yoder, D. A</creatorcontrib><title>Brush Seal Leakage Performance With Gaseous Working Fluids at Static and Low Rotor Speed Conditions</title><title>Journal of engineering for gas turbines and power</title><addtitle>J. Eng. Gas Turbines Power</addtitle><description>The leakage performance of a brush seal with gaseous working fluids at static and low rotor speed conditions was investigated. This report includes the leakage results for air, helium, and carbon dioxide at several bristle/rotor interferences. In addition, the effects of packing a lubricant into the bristles and also of reversing the pressure drop across the seal were investigated. Results were compared to that of an annular seal at similar operating conditions. In order to generalize the results, they were correlated using corresponding state theory. The brush seal tested had a bore diameter of 3.792 cm (1.4930 in.), a fence height of 0.0635 cm (0.025 in.), and 1800 bristles/cm-circumference (4500 bristles/in.-circumference). Various bristle/rotor radial interferences were achieved by using a tapered rotor. The brush seal reduced the leakage in comparison with the annular seal, up to 9.5 times. Reversing the pressure drop across the brush seal produced leakage rates approximately the same as that of the annular seal. Addition of a lubricant reduced the leakage by 2.5 times when compared to a nonlubricated brush seal. The air and carbon dioxide data were successfully correlated using the corresponding state theory. However, the helium data followed a different curve from the air and carbon dioxide data.</description><subject>20 FOSSIL-FUELED POWER PLANTS</subject><subject>200104 - Fossil-Fueled Power Plants- Components</subject><subject>330103 - Internal Combustion Engines- Turbine</subject><subject>ADVANCED PROPULSION SYSTEMS</subject><subject>AIR</subject><subject>Applied sciences</subject><subject>CARBON COMPOUNDS</subject><subject>CARBON DIOXIDE</subject><subject>CARBON OXIDES</subject><subject>CHALCOGENIDES</subject><subject>DATA</subject><subject>ELEMENTS</subject><subject>Energy</subject><subject>Energy. Thermal use of fuels</subject><subject>Engines and turbines</subject><subject>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</subject><subject>Exact sciences and technology</subject><subject>EXPERIMENTAL DATA</subject><subject>FLUID FLOW</subject><subject>FLUIDS</subject><subject>Gas engines</subject><subject>Gas turbines</subject><subject>GASES</subject><subject>HELIUM</subject><subject>INFORMATION</subject><subject>Leakage (fluid)</subject><subject>LUBRICANTS</subject><subject>NONMETALS</subject><subject>NUMERICAL DATA</subject><subject>OXIDES</subject><subject>OXYGEN COMPOUNDS</subject><subject>PERFORMANCE TESTING</subject><subject>Pressure measurement</subject><subject>RARE GASES</subject><subject>ROTORS</subject><subject>SEALS</subject><subject>SUBSONIC FLOW</subject><subject>TESTING</subject><subject>Thermal effects</subject><issn>0742-4795</issn><issn>1528-8919</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1993</creationdate><recordtype>article</recordtype><recordid>eNo9kE2LFDEURYMo2I4uXLsJIoiLGvNZSZbaOKPQoNjKLMPr1KvpzFQnPUkK8d9bQzeu3ubce3mHkNecXXLO9Ud-KRzrjRBPyIprYTvruHtKVswo0Snj9HPyotY7xriUyqxI-FzmuqdbhIluEO7hFukPLGMuB0gB6U1se3oNFfNc6U0u9zHd0qtpjkOl0Oi2QYuBQhroJv-hP3PLhW6PiANd5zTEFnOqL8mzEaaKr873gvy--vJr_bXbfL_-tv606UAa1jqUFiR3o2JScLETVuheWiUFszszBqEsKnCD1BZ3g9Vq7K0Qw86FIAP0S_aCvD315tqiryE2DPuQU8LQfK-Z0k4u0PsTdCz5Ycba_CHWgNME6fFHb1TPpOm5WsgPJzKUXGvB0R9LPED56znzj7I992fZC_vu3Ao1wDSWRV6s_wPKGq2dW7A3JwzqAf1dnktahHjFLFsG_wEGjoUk</recordid><startdate>19930401</startdate><enddate>19930401</enddate><creator>Carlile, J. A</creator><creator>Hendricks, R. C</creator><creator>Yoder, D. A</creator><general>ASME</general><general>American Society of Mechanical Engineers</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TC</scope><scope>OTOTI</scope></search><sort><creationdate>19930401</creationdate><title>Brush Seal Leakage Performance With Gaseous Working Fluids at Static and Low Rotor Speed Conditions</title><author>Carlile, J. A ; Hendricks, R. C ; Yoder, D. A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a370t-e38a319f403212b282563843208b7fc248e4a9d358ebd854f6822db9cc3ca68a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1993</creationdate><topic>20 FOSSIL-FUELED POWER PLANTS</topic><topic>200104 - Fossil-Fueled Power Plants- Components</topic><topic>330103 - Internal Combustion Engines- Turbine</topic><topic>ADVANCED PROPULSION SYSTEMS</topic><topic>AIR</topic><topic>Applied sciences</topic><topic>CARBON COMPOUNDS</topic><topic>CARBON DIOXIDE</topic><topic>CARBON OXIDES</topic><topic>CHALCOGENIDES</topic><topic>DATA</topic><topic>ELEMENTS</topic><topic>Energy</topic><topic>Energy. Thermal use of fuels</topic><topic>Engines and turbines</topic><topic>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</topic><topic>Exact sciences and technology</topic><topic>EXPERIMENTAL DATA</topic><topic>FLUID FLOW</topic><topic>FLUIDS</topic><topic>Gas engines</topic><topic>Gas turbines</topic><topic>GASES</topic><topic>HELIUM</topic><topic>INFORMATION</topic><topic>Leakage (fluid)</topic><topic>LUBRICANTS</topic><topic>NONMETALS</topic><topic>NUMERICAL DATA</topic><topic>OXIDES</topic><topic>OXYGEN COMPOUNDS</topic><topic>PERFORMANCE TESTING</topic><topic>Pressure measurement</topic><topic>RARE GASES</topic><topic>ROTORS</topic><topic>SEALS</topic><topic>SUBSONIC FLOW</topic><topic>TESTING</topic><topic>Thermal effects</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Carlile, J. A</creatorcontrib><creatorcontrib>Hendricks, R. C</creatorcontrib><creatorcontrib>Yoder, D. A</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical Engineering Abstracts</collection><collection>OSTI.GOV</collection><jtitle>Journal of engineering for gas turbines and power</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Carlile, J. A</au><au>Hendricks, R. C</au><au>Yoder, D. A</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Brush Seal Leakage Performance With Gaseous Working Fluids at Static and Low Rotor Speed Conditions</atitle><jtitle>Journal of engineering for gas turbines and power</jtitle><stitle>J. Eng. Gas Turbines Power</stitle><date>1993-04-01</date><risdate>1993</risdate><volume>115</volume><issue>2</issue><spage>397</spage><epage>403</epage><pages>397-403</pages><issn>0742-4795</issn><eissn>1528-8919</eissn><coden>JETPEZ</coden><abstract>The leakage performance of a brush seal with gaseous working fluids at static and low rotor speed conditions was investigated. This report includes the leakage results for air, helium, and carbon dioxide at several bristle/rotor interferences. In addition, the effects of packing a lubricant into the bristles and also of reversing the pressure drop across the seal were investigated. Results were compared to that of an annular seal at similar operating conditions. In order to generalize the results, they were correlated using corresponding state theory. The brush seal tested had a bore diameter of 3.792 cm (1.4930 in.), a fence height of 0.0635 cm (0.025 in.), and 1800 bristles/cm-circumference (4500 bristles/in.-circumference). Various bristle/rotor radial interferences were achieved by using a tapered rotor. The brush seal reduced the leakage in comparison with the annular seal, up to 9.5 times. Reversing the pressure drop across the brush seal produced leakage rates approximately the same as that of the annular seal. Addition of a lubricant reduced the leakage by 2.5 times when compared to a nonlubricated brush seal. The air and carbon dioxide data were successfully correlated using the corresponding state theory. However, the helium data followed a different curve from the air and carbon dioxide data.</abstract><cop>New York, NY</cop><pub>ASME</pub><doi>10.1115/1.2906722</doi><tpages>7</tpages><oa>free_for_read</oa></addata></record> |
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subjects | 20 FOSSIL-FUELED POWER PLANTS 200104 - Fossil-Fueled Power Plants- Components 330103 - Internal Combustion Engines- Turbine ADVANCED PROPULSION SYSTEMS AIR Applied sciences CARBON COMPOUNDS CARBON DIOXIDE CARBON OXIDES CHALCOGENIDES DATA ELEMENTS Energy Energy. Thermal use of fuels Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology EXPERIMENTAL DATA FLUID FLOW FLUIDS Gas engines Gas turbines GASES HELIUM INFORMATION Leakage (fluid) LUBRICANTS NONMETALS NUMERICAL DATA OXIDES OXYGEN COMPOUNDS PERFORMANCE TESTING Pressure measurement RARE GASES ROTORS SEALS SUBSONIC FLOW TESTING Thermal effects |
title | Brush Seal Leakage Performance With Gaseous Working Fluids at Static and Low Rotor Speed Conditions |
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