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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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