Gas turbine system

Power plants – Combustion products used as motive fluid – With addition of steam and/or water

Reexamination Certificate

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C060S728000

Reexamination Certificate

active

07367178

ABSTRACT:
A gas turbine system comprises a compressor for compressing air, a combustor for burning the air compressed by the compressor and fuel, a turbine driven by combustion gases produced from the combustor, and a spraying apparatus for adding water to working air at least upstream or in an intermediate stage of the compressor. A rotationally symmetric groove or projection is formed in an inner wall surface defining a channel through which the working air added with the water flows, or in a channel-defining surface of a rotor or a casing of the gas turbine. A larger amount of water can be supplied to the compressor while improving the reliability of the gas turbine.

REFERENCES:
patent: 5088280 (1992-02-01), Scott-Scott et al.
patent: 5669217 (1997-09-01), Anderson
patent: 7204670 (2007-04-01), Meher-Homji et al.
patent: 0889212 (1999-01-01), None
patent: 9-236024 (1997-09-01), None
patent: 2877098 (1998-01-01), None
patent: 2000-104562 (2000-04-01), None
patent: WO 03/071113 (2003-08-01), None
XP-002346415; Database WPI; Section PQ; Week 200029; Derwent Publications Ltd.; London; GB; Class Q52; AN 2000-333803; Apr. 11, 2000; Abstract.
“An Evaluation of the Effects of Water Injection on Compressor Performance” by A. White, et al. GT2003-38237, 2003, pp. 1-9.
“Inlet Fogging of Gas Turbine Engines-Part A: Fog Droplet Thermodynamics, Heat Transfer and Practical Considerations” by Mustapha Chaker, et al. GT-2002-30562, pp. 1-15, 2002.

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