发明名称 GAS TURBINE BLADE DAMPER
摘要 <p>An integrated damper and windage cover 52 has a windage cover portion 56 cantilevered at the upstream end, free of contact with the blade platform 24, 32. The contact portion 54 is rigid and bears against the underside of the blade platform 24, spanning blade platform clearance 50.</p>
申请公布号 EP0670956(B1) 申请公布日期 2000.05.31
申请号 EP19940901353 申请日期 1993.11.09
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CHLUS, WIESLAW, A.;GONSOR, MICHAEL;HOUSTON, DAVID, P.;KUDRA, PAUL, D.
分类号 F01D5/26;F01D5/22;F01D11/00;(IPC1-7):F01D5/26 主分类号 F01D5/26
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