发明名称 GAS TURBINE BLADE SEAL
摘要 An underplatform damper (52) contact portion (54) is rigid, and provides a loose seal between the underplatform cooling air (36) and the gas stream (40). At the aft end of the blade platform the pressure difference increases and a more effective seal is provided by a snap-in flexible seal (72).
申请公布号 WO9412772(A1) 申请公布日期 1994.06.09
申请号 WO1993US10682 申请日期 1993.11.04
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CHLUS, WIESLAW, A.
分类号 F01D5/26;F01D5/22;F01D11/00;(IPC1-7):F01D5/26 主分类号 F01D5/26
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