<p>A support arrangement for a brush seal (50) positioned between a stationary (40) and a rotatable (46) component of a turbomachine (10). The brush seal (50) has a downstream backing plate (54) that includes an axially-extending lip (70) adjacent its radially outermost end to minimize axial deflection of the seal (50) as a result of a gas pressure differential acting across the seal (50). <IMAGE></p>
申请公布号
EP1510655(B1)
申请公布日期
2007.07.25
申请号
EP20030255315
申请日期
2003.08.27
申请人
GENERAL ELECTRIC COMPANY
发明人
ALBERS, ROBERT JOSEPH;BAUER, RANDALL CHARLES;BRAUER, JOHN CHRISTOPHER;SCHMID, SCOTT JOSEPH;LEWIS, KENNETH MARTIN