Method for cooling a gas turbine system and a gas turbine...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S806000, C415S115000

Reexamination Certificate

active

09873373

ABSTRACT:
A gas turbine system comprises a compressor that takes in suction air on the inlet side and compresses it to compressor end air that is available on the outlet side, a combustor in which a fuel is burned by using the compressor end air while resulting in the formation of hot gas, as well as a turbine in which the hot gas is expanded while providing work output. In a method for cooling this gas turbine system, compressed air is removed from the compressor, is fed as cooling air for cooling inside an internal cooling channel through thermally loaded components of the combustor and/or the turbine, is then compressed and added to the compressor end air. An improved cooling without disadvantage for the efficiency of the system is achieved in that, in the manner of a targeted leakage, a small part of the cooling air is fed for film cooling into the turbine stream through drilled film cooling openings provided on the components.

REFERENCES:
patent: 3751909 (1973-08-01), Kohler
patent: 5392515 (1995-02-01), Auxier et al.
patent: 5498133 (1996-03-01), Lee
patent: 5581996 (1996-12-01), Koch et al.
patent: 5611197 (1997-03-01), Bunker
patent: 5782076 (1998-07-01), Huber et al.
patent: 5839271 (1998-11-01), Illbruck
patent: 6065282 (2000-05-01), Fukue et al.
patent: 6253554 (2001-07-01), Kobayashi et al.
patent: 6305155 (2001-10-01), Gross
patent: 197 37 845 (1999-03-01), None
patent: 198 32 767 (2000-01-01), None
patent: 0 392 664 (1990-10-01), None
patent: 0 899 425 (1999-03-01), None
patent: 1 001 136 (2000-05-01), None
patent: 1 149 983 (2001-10-01), None
patent: 1 162 355 (2001-12-01), None
patent: 0906531 (1997-03-01), None
patent: WO97/38219 (1997-10-01), None
patent: WO98/13584 (1998-04-01), None

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