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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	ZHENG XIAOQING, ADIS WILLIAM EDWARD, TURNQUIST NORMAN ARNOLD, BARAN ROBERT GERARD, PARKER KEITH MICHAEL, SARAWATE NEELESH NANDKUMAR, RODRIGUEZ ERDMENGER RODRIGO, PANNEKEET ROBBERT CHRISTIAAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	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
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Beschreibung
Zusammenfassung:	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.