发明名称 Gas Turbine Compressor Inlet Pressurization and Flow Control System
摘要 A supercharging system for a gas turbine system is provided supercharging system having a fan mechanically coupled to the turbine shaft of the turbine system. A bypass subsystem is provided or optionally conveying a portion of the airstream output to other uses. The supercharging system may also be used in conjunction with a combined cycle power system and a bypass subsystem optionally conveys a portion of the airstream output to a heat recovery steam generator.
申请公布号 US2013318997(A1) 申请公布日期 2013.12.05
申请号 US201213485216 申请日期 2012.05.31
申请人 CONCHIERI JOHN ANTHONY;THATCHER ROBERT THOMAS;RODWELL ANDREW MITCHELL;GENERAL ELECTRIC COMPANY 发明人 CONCHIERI JOHN ANTHONY;THATCHER ROBERT THOMAS;RODWELL ANDREW MITCHELL
分类号 F02C6/08 主分类号 F02C6/08
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