- Patent Title: Gas turbine compressor inlet pressurization and flow control system
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Application No.: US13485216Application Date: 2012-05-31
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Publication No.: US09771864B2Publication Date: 2017-09-26
- Inventor: John Anthony Conchieri , Robert Thomas Thatcher , Andrew Mitchell Rodwell
- Applicant: John Anthony Conchieri , Robert Thomas Thatcher , Andrew Mitchell Rodwell
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agent Ernest G. Cusick; Frank A. Landgraff
- Main IPC: F02C6/12
- IPC: F02C6/12
Abstract:
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.
Public/Granted literature
- US20130318997A1 Gas Turbine Compressor Inlet Pressurization and Flow Control System Public/Granted day:2013-12-05
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