发明名称 Abradable and/or abrasive coating and brush seal configuration
摘要 An abradable coating and/or an abrasive coating applied to the rotor of a steam or gas turbine allows the temperature and pressure drop capabilities of conventional brush seal assemblies to be increased. The pressure drop capability of brush seals is closely related to fence height, i.e., the distance between the rotor and the bottom edge of the backing plate supporting the brush seal wire bristles. Application of the abradable or abrasive coating allows the fence height to be reduced and the pressure capability of a brush seal assembly increased commensurately because the risk of the backing plate rubbing against the surface of the rotor, so as to cause damage to the rotor, is reduced. In addition, the backing plate can be made from a higher strength material that can withstand higher temperatures because any contact between the backing plate and the rotor results in no damage to the rotor, but rather a gradual reduction of the backing plate as it wears.
申请公布号 US2006249911(A1) 申请公布日期 2006.11.09
申请号 US20050121052 申请日期 2005.05.04
申请人 GENERAL ELECTRIC COMPANY 发明人 KOWALCZYK MARK W.;COUTURE BERNARD A.;RIVAS FLOR D.
分类号 F16J15/44 主分类号 F16J15/44
代理机构 代理人
主权项
地址