发明名称 Compliant brush shroud assembly for gas turbine engine compressors
摘要 <p>A brush shroud assembly for reducing the tip clearance between a rotating blade and an engine casing is disclosed. The assembly includes a plurality of bristle packs supported within a housing such that the bristle distribution at the inner diameter of the bristle packs is substantially continuous. The continuous surface is created by mounting the bristles packs within a housing such that the packs are flared, i.e. width at the outer diameter of the bristle pack is smaller than that at the inner diameter. Various embodiments are disclosed for mounting the flared bristle packs to form a substantially continuous inner diameter The bristle strips may be mounted in one or more annular rings, may be secured within one or more channels in the housing, the bristle packs may be formed into a tufted ring, or any of these may be utilized in combination with a backplate supporting an abradable seal, i.e. a hybrid design.</p>
申请公布号 GB2385098(A) 申请公布日期 2003.08.13
申请号 GB20030010262 申请日期 2001.11.05
申请人 * ADVANCED COMPONENTS & MATERIALS INC. 发明人 AMITAVA * DATTA
分类号 F01D11/08;F01D11/12;F02C7/28;F16J15/32;(IPC1-7):F16J15/447 主分类号 F01D11/08
代理机构 代理人
主权项
地址