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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
Main Authors: Carlile, J. A, Hendricks, R. C, Yoder, D. A
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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.
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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. 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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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identifier ISSN: 0742-4795
ispartof Journal of engineering for gas turbines and power, 1993-04, Vol.115 (2), p.397-403
issn 0742-4795
1528-8919
language eng
recordid cdi_osti_scitechconnect_6504593
source ASME Transactions Journals (Archives)
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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