发明名称 GAS TURBINE BLADE DAMPER
摘要 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).
申请公布号 WO9412773(A1) 申请公布日期 1994.06.09
申请号 WO1993US10803 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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