Gas turbine system having an air intake bypass system and an...

Power plants – Combustion products used as motive fluid – With exhaust treatment

Reexamination Certificate

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C060S039530

Reexamination Certificate

active

08069646

ABSTRACT:
A pressure vessel bypass valve forms a bypass system for enabling a part of the air compressed by a compressor to directly flow into a combustor while preventing the part of the air from flowing through a humidification tower and a recuperator. A turbine bypass valve forms another bypass system for enabling a part of a humidified air to be discharged to an exhaust duct after a heat exchange between the humidified air and a turbine exhaust gas is performed in the recuperator while preventing the part of the humidified air from flowing through a turbine. A turbine control system controls the bypass valves to be opened and closed in accordance with increase and decrease of the load.

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patent: 7444819 (2008-11-01), Shibata et al.
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patent: 61-066019 (1986-04-01), None
patent: 08-042360 (1996-02-01), None
patent: 2000-054857 (2000-02-01), None
patent: 2002-371860 (2002-12-01), None
patent: 2005-307861 (2005-11-01), None

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