US5740673A
Expired / Lapsed
US
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Operation of integrated gasification combined cycle power generation systems at part load
Assignee: Air Products and Chemicals Inc
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Filing: 1995-11-07
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Granted: 1998-04-21
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Expires: 2015-11-07
Abstract
Abstract An integrated gas turbine/air separation system is operated at or below full system load by feeding the air separation unit with air from a dedicated air feed compressor and optionally with extracted air from the gas turbine air compressor. When the gas turbine air compressor discharge drops below a selected pressure at part load conditions, the flow of extracted air to the air separation unit is discontinued and the air separation unit operates at constant pressure supplied only by the air feed compressor. This mode of operation is particularly useful in an integrated gasification combined cycle (IGCC) power generation system and allows the design of the oxygen and nitrogen product compressors such that the compressors operate at high efficiency during full load IGCC operation.
Inventors
- 👤 Arthur Ramsden Smith
- 👤 Donald Winston Woodward
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 06:27
CPC Classifications
F; F25; F25J; F25J3/00; F25J3/02; F25J3/04; F25J3/04006; F25J3/04109; F25J3/04115; F25J3/04127; F02; F02C; F02C1/00; F01; F01K; F01K23/00; F01K23/02; F01K23/06; F01K23/067; F01K23/068; F02C6/00; F25J3/04012; F25J3/04018; F25J3/0403; F25J3/04036; F25J3/04521; F25J3/04527; F25J3/04539; F25J3/04545; F25J3/04563; F25J3/04575; F25J3/04593; F25J3/04606; F25J3/04612; F25J3/04618; F25J3/04763; F25J3/04769; F25J3/04812; F25J3/04836; F25J2290/00; F25J2290/10; Y; Y02; Y02E; Y02E20/00; Y02E20/16; Y02E20/18
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
271 words
A method of operating an integrated gas turbine/air separation system at part load which comprises compressing a first stream of air in a gas turbine air compressor, combusting at least a portion of the resulting compressed air with a fuel in a gas turbine combustor to form hot combustion products, expanding the hot combustion products in a gas turbine expander which drives the compressor, separating air into nitrogen-rich and oxygen-rich products in a cryogenic air separation unit wherein feed air to the air separation unit is provided at least in part by compressing a second stream of air in a main air compressor, wherein the integrated gas turbine/air separation system is operated at part load such that (a) when the gas turbine air compressor supplies compressed air at a given operating pressure which is greater than a minimum air separation unit feed pressure, the air separation unit is operated at a feed pressure essentially equal to the given operating pressure and the feed air is provided to the air separation unit in part by the main air compressor and in part by an additional portion of compressed air from the gas turbine air compressor; and (b) when the gas turbine air compressor supplies compressed air at a given operating pressure which is essentially equal to or less than the minimum air separation unit feed pressure, the air separation unit is operated at a feed pressure essentially equal to the minimum air separation unit feed pressure and the feed air to the air separation unit is provided by the main air compressor without additional compressed air from the gas turbine air compressor.
Claim 2
Independent Claim
271 words
A method of operating an integrated gas turbine/air separation system at part load which comprises compressing a first stream of air in a gas turbine air compressor, combusting at least a portion of the resulting compressed air with a fuel in a gas turbine combustor to form hot combustion products, expanding the hot combustion products in a gas turbine expander which drives the compressor, separating air into nitrogen-rich and oxygen-rich products in a cryogenic air separation unit wherein feed air to the air separation unit is provided at least in part by compressing a second stream of air in a main air compressor, wherein the integrated gas turbine/air separation system is operated at part load such that (a) when the gas turbine air compressor supplies compressed air at a given operating pressure which is greater than a minimum air separation unit feed pressure, the air separation unit is operated at a feed pressure essentially equal to the given operating pressure and the feed air is provided to the air separation unit in part by the main air compressor and in part by an additional portion of compressed air from the gas turbine air compressor; and (b) when the gas turbine air compressor supplies compressed air at a given operating pressure which is essentially equal to or less than the minimum air separation unit feed pressure, the air separation unit is operated at a feed pressure essentially equal to the minimum air separation unit feed pressure and the feed air to the air separation unit is provided by the main air compressor without additional compressed air from the gas turbine air compressor.
Claim 3
Dependent Claim
19 words
The method of claim 1 wherein the minimum air separation unit feed pressure is between 80 and 500 psia.
Claim 4
Dependent Claim
139 words
The method of claim 1 wherein the main air compressor operates such that (c) when the main air compressor operates at a discharge pressure which is greater than the minimum air separation unit feed pressure, the main air compressor is operated above its minimum design total relative compression ratio and below its maximum design relative suction volume flow; and (d) when the main air compressor operates at a discharge pressure which is essentially equal to the minimum air separation unit feed pressure, the main air compressor is operated essentially at its minimum design total relative compression ratio and at or below its maximum design relative suction volume flow; wherein the minimum design total relative compression ratio and the maximum design relative suction volume flow of the main air compressor occur essentially at the minimum air separation unit feed pressure.
Claim 5
Dependent Claim
20 words
The method of claim 3 wherein the main air compressor operates at a discharge pressure between 80 and 600 psia.
Claim 6
Dependent Claim
156 words
The method of claim 1 which further comprises compressing the oxygen-rich product in an oxygen compressor which operates such that (e) when the main air compressor operates at a discharge pressure which is greater than the minimum air separation unit feed pressure, the oxygen compressor is operated below its maximum design total relative compression ratio and below its maximum design relative suction volume flow; and (f) when the main air compressor operates at a discharge pressure which is essentially equal to the minimum air separation unit feed pressure, the oxygen compressor is operated essentially at its maximum design total relative compression ratio and at or below its maximum design relative suction volume flow; wherein the maximum design total relative compression ratio and the maximum design relative suction volume flow of the oxygen compressor occur when the main air compressor operates at a discharge pressure which is essentially equal to the minimum air separation unit feed pressure.
Claim 7
Dependent Claim
19 words
The method of claim 5 wherein the oxygen compressor operates at a discharge pressure between 120 and 2000 psia.
Claim 8
Dependent Claim
30 words
The method of claim 5 which further comprises generating the fuel for the gas turbine combustor by gasifying a carbonaceous feedstock with compressed oxygen-rich product from the air separation unit.
Claim 9
Dependent Claim
31 words
The method of claim 7 which further comprises compressing at least a portion of the nitrogen-rich product in a nitrogen compressor for use in the process for gasifying the carbonaceous feedstock.
Claim 10
Dependent Claim
147 words
The method of claim 8 wherein the nitrogen compressor operates such that (g) when the main air compressor operates at a discharge pressure which is greater than the minimum air separation unit feed pressure, the nitrogen compressor is operated below its maximum design total relative compression ratio and below its maximum design relative suction volume flow; and (h) when the main air compressor operates at a discharge pressure which is essentially equal to the minimum air separation unit feed pressure, the nitrogen compressor is operated essentially at its maximum design total relative compression ratio and at or below its maximum design relative suction volume flow; wherein the maximum design total relative compression ratio and the maximum design relative suction volume flow the nitrogen compressor occur when the main air compressor operates at a discharge pressure which is essentially equal to the minimum air separation unit feed pressure.
Claim 11
Dependent Claim
19 words
The method of claim 9 wherein the nitrogen compressor operates at a discharge pressure between 50 and 2000 psia.
Claim 12
Dependent Claim
32 words
The method of claim 1 which further comprises compressing at least a portion of the nitrogen-rich product in a nitrogen compressor and introducing the resulting compressed nitrogen into the gas turbine combustor.
Claim 13
Dependent Claim
147 words
The method of claim 11 wherein the nitrogen compressor operates such that (i) when the main air compressor operates at a discharge pressure which is greater than the minimum air separation unit feed pressure, the nitrogen compressor is operated below its maximum design total relative compression ratio and below its maximum design relative suction volume flow; and (j) when the main air compressor operates at a discharge pressure which is essentially equal to the minimum air separation unit feed pressure, the nitrogen compressor is operated essentially at its maximum design total relative compression ratio and at or below its maximum design relative suction volume flow; wherein the maximum design total relative compression ratio and the maximum design relative suction volume flow the nitrogen compressor occur when the main air compressor operates at a discharge pressure which is essentially equal to the minimum air separation unit feed pressure.
Claim 14
Dependent Claim
19 words
The method of claim 12 wherein the nitrogen compressor operates at a discharge pressure between 120 and 2000 psia.
Claim 15
Dependent Claim
19 words
The method of claim 1 wherein the gas turbine expander which drives the compressor also drives an electric generator.
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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) | 2001-04-20 | 2001-10-20 | 2002-04-21 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2005-04-20 | 2005-10-20 | 2006-04-21 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2009-04-20 | 2009-10-20 | 2010-04-21 | $7700.00 | Window Closed / Lapsed |