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Patent US5083423A successfully refreshed from Google Patents.
US5083423A
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US
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Apparatus and method for optimizing the air inlet temperature of gas turbines
Assignee: S and S Trust
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Filing: 1990-04-26
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Granted: 1992-01-28
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Expires: 2010-04-26
Abstract
Abstract A heat exchanger is disclosed for heating air entering a combustion gas turbine to increase the power output of the turbine when the turbine operates in a cold environment. The heat exchanger may be used also as a cooler to cool air entering the turbine to increase the power output of the turbine when the turbine operates in a hot environment.
Inventors
- 👤 James K. Prochaska
- 👤 Mark H. Axford
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 09:04
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/08; F02C7/04; F02C7/12; F02C7/14; F02C7/141; F02C7/143; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 14
Claim 1
Independent Claim
47 words
A method of increasing the power output of a combustion gas turbine which utilizes air and has a compression section, a combustion section and an expansion section, comprising the step of heating the air indirectly prior to flowing the air to the compression section of the turbine.
Claim 2
Independent Claim
47 words
A method of increasing the power output of a combustion gas turbine which utilizes air and has a compression section, a combustion section and an expansion section, comprising the step of heating the air indirectly prior to flowing the air to the compression section of the turbine.
Claim 3
Independent Claim
48 words
A method of increasing the power output of a multi-shaft combustion gas turbine which utilizes air and has a compression section, a combustion section and an expansion section, comprising the step of heating the air indirectly prior to flowing the air into the compression section of the turbine.
Claim 4
Independent Claim
48 words
A method of increasing the power output of a multi-shaft combustion gas turbine which utilizes air and has a compression section, a combustion section and an expansion section, comprising the step of heating the air indirectly prior to flowing the air into the compression section of the turbine.
Claim 5
Dependent Claim
20 words
A method according to claim 2 wherein the heating step includes the step of exchanging heat with a heating medium.
Claim 6
Dependent Claim
118 words
In a multi-shaft combustion gas turbine which has a compression section, a combustion section and an expansion section and whose power output is affected by the temperature of air entering the turbine so that the power output reaches its maximum at an optimum temperature of the air entering the turbine and decreases as the temperature of the air entering the turbine decreases below or increases above the optimum temperature, a method of increasing the power output of the turbine, comprising the step of heating the air indirectly prior to entering the compression section of the turbine to increase the temperature of the air towards the optimum temperature, if the temperature of the air is below the optimum temperature.
Claim 7
Dependent Claim
118 words
In a multi-shaft combustion gas turbine which has a compression section, a combustion section and an expansion section and whose power output is affected by the temperature of air entering the turbine so that the power output reaches its maximum at an optimum temperature of the air entering the turbine and decreases as the temperature of the air entering the turbine decreases below or increases above the optimum temperature, a method of increasing the power output of the turbine, comprising the step of heating the air indirectly prior to entering the compression section of the turbine to increase the temperature of the air towards the optimum temperature, if the temperature of the air is below the optimum temperature.
Claim 8
Dependent Claim
60 words
In a multi-shaft combustion gas turbine which receives air and whose power output is affected by the temperature of the air, a method of maximizing the power output of the turbine comprising the step of raising or lowering the temperature of the air being received by the turbine prior to flowing the air to a compression section of the turbine.
Claim 9
Dependent Claim
60 words
In a multi-shaft combustion gas turbine which receives air and whose power output is affected by the temperature of the air, a method of maximizing the power output of the turbine comprising the step of raising or lowering the temperature of the air being received by the turbine prior to flowing the air to a compression section of the turbine.
Claim 10
Dependent Claim
32 words
A method according to claim 5 wherein the raising or lowering step includes the step of exchanging heat between the air and a heating or a cooling medium in a heat exchanger.
Claim 11
Dependent Claim
107 words
In a combustion gas turbine wherein the air inlet temperature of the air flowing into the turbine has an effect on the power output of the turbine, the effect being characterized by a maximum power output at an optimum air inlet temperature and a decrease as the air inlet temperature increases above or decreases below the optimum air inlet temperature, a method of increasing the power output of the turbine, comprising the step of cooling the air, if the temperature of the air is above the optimum air inlet temperature or heating the air, if the temperature of the air is below the optimum air inlet temperature.
Claim 12
Dependent Claim
107 words
In a combustion gas turbine wherein the air inlet temperature of the air flowing into the turbine has an effect on the power output of the turbine, the effect being characterized by a maximum power output at an optimum air inlet temperature and a decrease as the air inlet temperature increases above or decreases below the optimum air inlet temperature, a method of increasing the power output of the turbine, comprising the step of cooling the air, if the temperature of the air is above the optimum air inlet temperature or heating the air, if the temperature of the air is below the optimum air inlet temperature.
Claim 13
Independent Claim
113 words
A method of increasing the power output of a combustion gas turbine which has a compression section, a combustion section and an expansion section and wherein the air inlet temperature of the air flowing into the turbine has an effect on the power output of the turbine, the effect being characterized by a maximum power output at an optimum air inlet temperature and a decrease as the air inlet temperature increases above or decreases below the optimum air inlet temperature, said method comprising the step of heating the air indirectly prior to flowing the air to the compression section, if the temperature of the air is less than the optimum air inlet temperature.
Claim 14
Independent Claim
113 words
A method of increasing the power output of a combustion gas turbine which has a compression section, a combustion section and an expansion section and wherein the air inlet temperature of the air flowing into the turbine has an effect on the power output of the turbine, the effect being characterized by a maximum power output at an optimum air inlet temperature and a decrease as the air inlet temperature increases above or decreases below the optimum air inlet temperature, said method comprising the step of heating the air indirectly prior to flowing the air to the compression section, if the temperature of the air is less than the optimum air inlet temperature.
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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) | 1995-01-27 | 1995-07-29 | 1996-01-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-01-27 | 1999-07-29 | 2000-01-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-01-27 | 2003-07-29 | 2004-01-28 | $7700.00 | Window Closed / Lapsed |