Axial brush seal
A brush seal assembly (100) for turbo machinery having a rotor can include a stationary seal component (105), a floating seal component (110) coupled to the stationary seal component and circumferentially angled bristles (120) arranged in a bristle pack, disposed in the floating seal component and e...
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| creator | ZHENG XIAOQING ADIS WILLIAM EDWARD TURNQUIST NORMAN ARNOLD BARAN ROBERT GERARD PARKER KEITH MICHAEL SARAWATE NEELESH NANDKUMAR RODRIGUEZ ERDMENGER RODRIGO PANNEKEET ROBBERT CHRISTIAAN |
| description | A brush seal assembly (100) for turbo machinery having a rotor can include a stationary seal component (105), a floating seal component (110) coupled to the stationary seal component and circumferentially angled bristles (120) arranged in a bristle pack, disposed in the floating seal component and extended axially with respect to the rotor. |
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PANNEKEET ROBBERT CHRISTIAAN</creatorcontrib><description>A brush seal assembly (100) for turbo machinery having a rotor can include a stationary seal component (105), a floating seal component (110) coupled to the stationary seal component and circumferentially angled bristles (120) arranged in a bristle pack, disposed in the floating seal component and extended axially with respect to the rotor.</description><language>chi ; eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; CYLINDERS ; ENGINE PLANTS IN GENERAL ; ENGINEERING ELEMENTS AND UNITS ; GAS-TURBINE PLANTS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PISTONS ; SEALINGS ; STEAM ENGINES ; 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ADIS WILLIAM EDWARD ; TURNQUIST NORMAN ARNOLD ; BARAN ROBERT GERARD ; PARKER KEITH MICHAEL ; SARAWATE NEELESH NANDKUMAR ; RODRIGUEZ ERDMENGER RODRIGO ; PANNEKEET ROBBERT CHRISTIAAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN103403300A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2013</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>CYLINDERS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PISTONS</topic><topic>SEALINGS</topic><topic>STEAM ENGINES</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHENG XIAOQING</creatorcontrib><creatorcontrib>ADIS WILLIAM EDWARD</creatorcontrib><creatorcontrib>TURNQUIST NORMAN ARNOLD</creatorcontrib><creatorcontrib>BARAN ROBERT GERARD</creatorcontrib><creatorcontrib>PARKER KEITH MICHAEL</creatorcontrib><creatorcontrib>SARAWATE NEELESH NANDKUMAR</creatorcontrib><creatorcontrib>RODRIGUEZ ERDMENGER RODRIGO</creatorcontrib><creatorcontrib>PANNEKEET ROBBERT CHRISTIAAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHENG XIAOQING</au><au>ADIS WILLIAM EDWARD</au><au>TURNQUIST NORMAN ARNOLD</au><au>BARAN ROBERT GERARD</au><au>PARKER KEITH MICHAEL</au><au>SARAWATE NEELESH NANDKUMAR</au><au>RODRIGUEZ ERDMENGER RODRIGO</au><au>PANNEKEET ROBBERT CHRISTIAAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Axial brush seal</title><date>2013-11-20</date><risdate>2013</risdate><abstract>A brush seal assembly (100) for turbo machinery having a rotor can include a stationary seal component (105), a floating seal component (110) coupled to the stationary seal component and circumferentially angled bristles (120) arranged in a bristle pack, disposed in the floating seal component and extended axially with respect to the rotor.</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN103403300A |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS CYLINDERS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GAS-TURBINE PLANTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PISTONS SEALINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS |
| title | Axial brush seal |
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