发明申请
US20130318997A1 Gas Turbine Compressor Inlet Pressurization and Flow Control System 有权
燃气轮机压缩机入口加压和流量控制系统

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.
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