Patent US3677409A successfully refreshed from Google Patents.
US5363642A
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Method of operating a gas turbine group
Assignee: Alstom SA
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Filing: 1994-02-25
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Granted: 1994-11-15
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Expires: 2014-02-25
Abstract
Abstract In a method of operating a gas turbine group (34) with or without integrated steam process (20) and with or without an air reservoir installation (20), a series connection with one and the same air mass flow (16, 17) is used for cooling one or more structures (15, 18, 19) which are in effective connection with the mass flow of the gas turbine group (34), the cooling air mass flow being extracted from a position which has a sufficiently low temperature.
Inventors
- 👤 Hans U. Frutschi
- 👤 Anders Lindvall
- 👤 Hans Wettstein
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 21:36
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/12; F02C7/16; F02C7/18; F02C1/00; F02C6/00; F02C6/14; F02C6/16; F05; F05D; F05D2260/00; F05D2260/20; F05D2260/211; Y; Y02; Y02E; Y02E20/00; Y02E20/14; Y02E60/00; Y02E60/16
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
204 words
A method of operating a gas turbine group, the gas turbine group comprising a high pressure and a low pressure compressor, an intercooler operating between the compressors, at least a first high pressure and a second low pressure gas turbine, the first gas turbine upstream of the second gas turbine, and at least one electrical machine, the method comprising the steps of: operating a first heat generator upstream of the first gas turbine to generate a hot mass flow for driving the first gas turbine; operating a further heat generator downstream of the first turbine and upstream of the second gas turbine to further heat the mass flow for driving the second gas turbine; extracting a single stream of compressed air from the high pressure compressor upstream of its outlet; directing the single flow of compressed air in series to at least two components of the gas turbine group through which the hot mass flow moves for cooling the components, at least a first component being cooled by providing the compressed air to the component without mixing the compressed cooling air with the hot mass flow; and, upon cooling a final component in series, admixing the compressed air in with the hot mass flow.
Claim 2
Independent Claim
204 words
A method of operating a gas turbine group, the gas turbine group comprising a high pressure and a low pressure compressor, an intercooler operating between the compressors, at least a first high pressure and a second low pressure gas turbine, the first gas turbine upstream of the second gas turbine, and at least one electrical machine, the method comprising the steps of: operating a first heat generator upstream of the first gas turbine to generate a hot mass flow for driving the first gas turbine; operating a further heat generator downstream of the first turbine and upstream of the second gas turbine to further heat the mass flow for driving the second gas turbine; extracting a single stream of compressed air from the high pressure compressor upstream of its outlet; directing the single flow of compressed air in series to at least two components of the gas turbine group through which the hot mass flow moves for cooling the components, at least a first component being cooled by providing the compressed air to the component without mixing the compressed cooling air with the hot mass flow; and, upon cooling a final component in series, admixing the compressed air in with the hot mass flow.
Claim 3
Dependent Claim
89 words
The method as claimed in claim 1, wherein the gas turbine group further comprises an air reservoir installation, wherein, during operation of the gas turbine group with the air reservoir as a source of compressed air, the method further comprising the steps of: discharging compressed air from the air reservoir installation through a supply conduit located downstream of the high pressure compressor and upstream of the first heat generator; and, extracting air required for cooling downstream of the reservoir and directing the extracted air to the components for cooling.
Claim 4
Dependent Claim
30 words
The method as claimed in claim 2, wherein a heat exchanger acts downstream of the reservoir and wherein the air required for cooling is extracted downstream of this heat exchanger.
Claim 5
Dependent Claim
19 words
The method as claimed in claim 1, wherein a high-pressure turbine and a low-pressure turbine are cooled in series.
Claim 6
Dependent Claim
17 words
The method as claimed in claim 4, wherein the stators of the turbines are cooled in series.
Claim 7
Dependent Claim
23 words
The method as claimed in claim 1, wherein the heat generator at the low-pressure end and the low-pressure turbine are cooled in series.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1997-11-14 | 1998-05-16 | 1998-11-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2001-11-14 | 2002-05-16 | 2002-11-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2005-11-14 | 2006-05-16 | 2006-11-15 | $7700.00 | Window Closed / Lapsed |