发明名称 Compressor interstage seal
摘要 <p>An interstage seal (24) for a gas turbine engine includes a seal pad (30) attached to a backing strip (28). A plurality of tab springs (32) are fixedly attached to the outboard side of the strip for engaging an inner band of the supporting stator sector. &lt;IMAGE&gt;</p>
申请公布号 EP0980963(A2) 申请公布日期 2000.02.23
申请号 EP19990306482 申请日期 1999.08.17
申请人 GENERAL ELECTRIC COMPANY 发明人 SCHILLING, JAN CHRISTOPHER
分类号 F04D29/08;F01D11/00;F04D17/10;(IPC1-7):F01D11/00 主分类号 F04D29/08
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