发明名称 GAS TURBINE TRANSITION PIECE AIR BYPASS BAND ASSEMBLY
摘要 An air bypass band assembly includes a transition piece of a gas turbine, the transition piece having at least one opening therein to allow a flow of air to pass through the at least one opening. The air bypass band assembly also includes a band that is movable between at least two positions, a first one of the at least two positions being a closed position where the at least one opening is closed to prevent the flow of air from flowing through the at least one opening, a second one of the at least two positions being an open where the at least one opening is opened to allow the flow of air to flow through the at least one opening. The air bypass band assembly further includes a mechanism that moves the band between the at least two positions.
申请公布号 US2011173984(A1) 申请公布日期 2011.07.21
申请号 US20100917561 申请日期 2010.11.02
申请人 GENERAL ELECTRIC COMPANY 发明人 VALEEV ALMAZ;GINESSIN LEONID;MESHKOV SERGEY ANATOLIEVICH
分类号 F01D25/24 主分类号 F01D25/24
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