发明名称 Gas turbine steam passage seal structure between blade ring and stationary blade
摘要 Gas turbine steam passage seal structure between a blade ring and a stationary blade absorbs thermal deformation to prevent occurrence of minute gaps to thereby reduce leakage of steam as cooling medium. A blade ring steam passage hole, provided in the blade ring (10), has a stepped portion formed in a middle portion thereof. A stationary blade steam passage hole, provided in the stationary blade (50) so as to oppose the blade ring steam passage hole, has a stepped portion formed in an outer peripheral portion thereof. A cooling steam supply passage connection portion is constructed comprising a seal pipe (25) provided between the blade ring and stationary blade steam passage holes so as to communicate them with each other and a seal urging guide device (44, 47) provided at each of the stepped portions of the blade ring and stationary blade steam passage holes so as to effect a seal while fixedly supporting the seal pipe (25). Leakage of the steam is reduced, temperature lowering of combustion gas is prevented, drive force of a steam turbine is increased and the entire thermal efficiency of the combined cycle power plant can be enhanced.
申请公布号 US2002076319(A1) 申请公布日期 2002.06.20
申请号 US20010988720 申请日期 2001.11.20
申请人 OYA TAKEAKI;HIROKAWA KAZUHARU;TANIOKA TADATERU;KUNITAKE NOBUHIRO 发明人 OYA TAKEAKI;HIROKAWA KAZUHARU;TANIOKA TADATERU;KUNITAKE NOBUHIRO
分类号 F01D9/02;F01D9/06;F01D11/00;F02C7/18;F02C7/28;(IPC1-7):F01D5/14 主分类号 F01D9/02
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