发明名称 Abradable seals
摘要 A sealing element (30) for a turbine of a gas turbine engine includes a radially inner surface region provided with an integrally formed seal structure (38) comprising a plurality of radially inwardly projecting walls (40). The walls may be abradable and may define cells (44) for receiving an abradable sealing material.
申请公布号 US2001031201(A1) 申请公布日期 2001.10.18
申请号 US20010815041 申请日期 2001.03.23
申请人 LAWER STEVEN D.;HALLIWELL MARK A. 发明人 LAWER STEVEN D.;HALLIWELL MARK A.
分类号 F01D11/12;F16J15/44;(IPC1-7):F01D11/12 主分类号 F01D11/12
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