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US6178735B1 Expired / Lapsed US ⏱️ 0.0 years remaining

Combined cycle power plant

Assignee: Alstom SA
•
Filing: 1998-12-10
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Granted: 2001-01-30
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Expires: 2018-12-10
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Abstract

Abstract In a method for operating a gas turbo-generator set (GT), the caloric potential of the exhaust gases ( 14 ) from the gas turbo-generator set (GT) is utilized by guiding them through a heat exchanger ( 5 ) which is operatively connected to a hot-air turbo-generator set (LT). A compressor ( 7 ) associated with this hot-air turbo-generator set (LT) is operated isothermally by means of point-focused or continuous water injection ( 24 ), and, after expansion ( 6 ) has taken place, the injected water is collected by condensation ( 19 ) in a separator ( 10 ). A circuit is thus provided, in which the adaptation of assemblies in order to achieve maximized efficiency is avoided.

Inventors

  • 👤 Hans Ulrich Frutschi

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 18:20
CPC Classifications
F; F02; F02C; F02C1/00; F02C1/04; F02C1/10; F01; F01K; F01K21/00; F01K21/04; F02C1/007; F02C6/00; F02C6/18; F02C7/00; F02C7/12; F02C7/14; F02C7/141; F02C7/143; F02C7/1435; Y; Y02; Y02E; Y02E20/00; Y02E20/16

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 91 words
A method for operating a gas turbo-generator set with single stage or multistage combustion, comprising the steps of providing a heat exchanger for further utilization of the caloric potential of exhaust gases from a turbine associated with the gas turbo-generator set, wherein a hot-air turbo-generator set is operatively connected to the heat exchanger; approximately simulating isothermal compression by water injection which is carried out in a compressor associated with the hot-air turbo-generator set; and after expansion has taken place by an expander, collecting the injected water by condensation in a separator.
Claim 2
Independent Claim 91 words
A method for operating a gas turbo-generator set with single stage or multistage combustion, comprising the steps of providing a heat exchanger for further utilization of the caloric potential of exhaust gases from a turbine associated with the gas turbo-generator set, wherein a hot-air turbo-generator set is operatively connected to the heat exchanger; approximately simulating isothermal compression by water injection which is carried out in a compressor associated with the hot-air turbo-generator set; and after expansion has taken place by an expander, collecting the injected water by condensation in a separator.
Claim 3
Independent Claim 23 words
The method as claimed in claim l, wherein the water is collected in the separator is recirculated for water injection into the compressor.
Claim 4
Dependent Claim 46 words
The method as claim in claim 1 , wherein part of the air occurring from the separator is introduced into the intake air of a compressor associated with the gas turbo-generator set or into the process air of a turbomachine associated with the gas turbo-generator set.
Claim 5
Dependent Claim 25 words
The method as claimed in claim 1 , wherein the air occurring in the separator is introduced into the compressor of the hot-air turbo-generator set.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 2004-01-30 2004-07-31 2005-01-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2008-01-30 2008-07-31 2009-01-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2012-01-30 2012-07-31 2013-01-30 $7700.00 Window Closed / Lapsed

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