Patent US5095693A successfully refreshed from Google Patents.
US5095693A
Expired / Lapsed
US
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High-efficiency gas turbine engine
Assignee: RTX Corp
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Filing: 1991-05-13
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Granted: 1992-03-17
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Expires: 2011-05-13
Abstract
Abstract A high efficiency/low nitric oxide emission gas turbine engine includes an interchanger for cooling a compressed air side stream which is used for cooling the turbine section. The heated fuel is then mixed with steam for injection into a combustor, thereby reducing nitric oxide emissions, while preventing condensation during mixing. Where water is used for injection instead of steam, both the fuel and water are preheated by interchange with the hot compressed gas stream. Preheating the fuel and/or water prevents steam condensate or water from entering the combustor, and does so using heat available within the gas turbine cycle thereby increasing overall turbine efficiency. In addition, utilizing a fuel/air interchanger reduces the size of the heat exchanger and the need for other auxiliary equipment, reducing costs while increasing turbine efficiency.
Inventors
- 👤 William H. Day
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 16:13
CPC Classifications
F; F02; F02C; F02C3/00; F02C3/20; F02C3/30; F02C7/00; F02C7/12; F02C7/14; F02C7/141; F02C7/22; F02C7/224; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
146 words
A high efficient gas turbine engine, having compression means, combustion means, turbine means, and means for reducing nitrous oxide emissions from an exhaust gas stream exiting from the turbine means, the engine further comprising: interchange means in fluid communication with a hot compressed air stream exiting from the compressor means, for cooling the compressed air stream as it passes therethrough; means for delivering the cooled compressed air stream to the turbine means for cooling the turbine means, a fuel, in fluid communication with the interchange means, and separability passable therethrough, the fuel heated by the hot compressed air stream prior to entering the combustion means and, pre-mixer means for reducing the nitrous oxide emissions, the heated fuel entering the pre-mixer means and mixed with steam prior to entering the combustion means, the entering fuel being at a temperature which prevents condensation of the steam during mixing.
Claim 2
Dependent Claim
146 words
A high efficient gas turbine engine, having compression means, combustion means, turbine means, and means for reducing nitrous oxide emissions from an exhaust gas stream exiting from the turbine means, the engine further comprising: interchange means in fluid communication with a hot compressed air stream exiting from the compressor means, for cooling the compressed air stream as it passes therethrough; means for delivering the cooled compressed air stream to the turbine means for cooling the turbine means, a fuel, in fluid communication with the interchange means, and separability passable therethrough, the fuel heated by the hot compressed air stream prior to entering the combustion means and, pre-mixer means for reducing the nitrous oxide emissions, the heated fuel entering the pre-mixer means and mixed with steam prior to entering the combustion means, the entering fuel being at a temperature which prevents condensation of the steam during mixing.
Claim 3
Dependent Claim
28 words
The gas turbine engine of claim 1 wherein the interchange means comprise a heat exchanger, heat transferred between the compressed air and the fuel in a non-contact manner.
Claim 4
Dependent Claim
14 words
The gas turbine engine of claim 1 wherein the fuel is a gaseous fuel.
Claim 5
Dependent Claim
14 words
The gas turbine engine of claim l wherein the fuel is a liquid fuel.
Claim 6
Dependent Claim
52 words
The gas turbine engine of claim 1 wherein the interchange means is a first heat exchanger; and, further comprising a second heat exchanger, in fluid communication with the compressed air stream, and separably, in fluid communication with a water stream, for transferring heat from the compressed air stream to the water stream.
Claim 7
Dependent Claim
111 words
The gas turbine engine of claim 1 wherein the interchange means comprise a closed loop heat transfer system including an inert fluid; pump means for recirculating the inert fluid; a reservoir for containing a portion of the fluid; first heat exchanger means, through which the fluid is passed, the compressed air stream separably passed through the first heat exchanger means, wherein the fluid is heated thereby; second heat exchanger means through which the fluid exiting from the first heat exchange means is passed, the fuel separably passed through the second heat exchanger means, wherein the fuel is heated to a desired temperature, the fluid then returned to the reservoir for recycling.
Claim 8
Dependent Claim
21 words
The gas turbine engine of claim 5 wherein the compressed air travels through the first and second heat exchangers in parallel.
Claim 9
Dependent Claim
50 words
The gas turbine engine of claim 6 further comprising a third heat exchange means, the fluid, exiting from the first heat exchange means which is in fluid communication with the third heat exchange means, passing therethrough; and, water, separably passed through the third heat exchange means, and being heated thereby.
Claim 10
Independent Claim
136 words
A method for operating a gas turbine engine having compression means, combustion means, and turbine means, the method comprising: providing interchange means in fluid communication with a hot compressed air stream exiting from the compressor means; passing the compressed air stream through the interchange means for reducing the temperature of the compressed air stream; delivering the cooled compressed air stream to the turbine means for cooling the turbine means; passing a fuel, separably, through the interchange means for heating the fuel using the hot compressed air stream; providing pre-mixer means for reducing nitrous oxide emissions from the exhaust gas stream exiting from the turbine means; and, mixing the heated fuel in the pre-mixer means with steam prior to entering the combustion means, the fuel being at a temperature which prevents condensation of the steam during mixing.
Claim 11
Independent Claim
136 words
A method for operating a gas turbine engine having compression means, combustion means, and turbine means, the method comprising: providing interchange means in fluid communication with a hot compressed air stream exiting from the compressor means; passing the compressed air stream through the interchange means for reducing the temperature of the compressed air stream; delivering the cooled compressed air stream to the turbine means for cooling the turbine means; passing a fuel, separably, through the interchange means for heating the fuel using the hot compressed air stream; providing pre-mixer means for reducing nitrous oxide emissions from the exhaust gas stream exiting from the turbine means; and, mixing the heated fuel in the pre-mixer means with steam prior to entering the combustion means, the fuel being at a temperature which prevents condensation of the steam during mixing.
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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) | 1995-03-17 | 1995-09-16 | 1996-03-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-03-17 | 1999-09-16 | 2000-03-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-03-17 | 2003-09-16 | 2004-03-17 | $7700.00 | Window Closed / Lapsed |