US4660376A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for operating a fluid injection gas turbine engine
Assignee: General Electric Co
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Filing: 1985-10-21
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Granted: 1987-04-28
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Expires: 2005-10-21
Abstract
Abstract A gas turbine including at least a compressor, a combustor, and a turbine is constructed to operate at a preferred thermal efficiency in predetermined compressor and turbine flow pressure ratios. A fluid, such as steam, for example produced by waste heat and pressurized as water, and characterized as having a higher specific heat at constant pressure than effluent from the combustor is introduced into such effluent to provide a turbine operating medium of improved potential to transfer energy downstream of the combustor. Such injection provides effective variable geometry to the system. This injection system maintains such pressure flow ratios substantially independent of engine power output.
Inventors
- 👤 Kenneth O. Johnson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 20:21
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/16; F01; F01K; F01K21/00; F01K21/04; F01K21/047; F05; F05D; F05D2260/00; F05D2260/20; F05D2260/232; F05D2260/2322; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
236 words
In a method of operating a gas turbine engine system comprising a gas turbine engine which includes, in operating series, a compressor having a compressor inlet, a combustor generating a gaseous combustor effluent, and a turbine, the system including compressor sensing means, turbine sensing means, a system control, a supply of fluid based on at least one form of water and having a specific heat at constant pressure (Cp) greater than the combustor effluent, and fluid introductory means to introduce the fluid from the supply of fluid into the engine, the steps of: designing and constructing the engine to operate as a gas turbine engine, without introduction of the fluid, at a preferred thermal efficiency range in a predetermined compressor flow pressure ratio range and a predetermined turbine flow pressure ratio range; sensing, during engine operation, with the compressor sensing means, actual compressor operating parameters sufficient to identify the operating compressor flow pressure ratio; sensing, during engine operation, with the turbine sensing means, actual turbine operating parameters sufficient to identify the operating turbine flow pressure ratio; comparing the sensed actual operating compressor flow and turbine flow pressure ratios with the predetermined compressor flow and turbine flow pressure ratio ranges; and then introducing and modulating the fluid into the engine through the fluid introduction means downstream of the compressor inlet as required to maintain the compressor and the turbine flow pressure ratios in their respective predetermined ranges.
Claim 2
Dependent Claim
236 words
In a method of operating a gas turbine engine system comprising a gas turbine engine which includes, in operating series, a compressor having a compressor inlet, a combustor generating a gaseous combustor effluent, and a turbine, the system including compressor sensing means, turbine sensing means, a system control, a supply of fluid based on at least one form of water and having a specific heat at constant pressure (Cp) greater than the combustor effluent, and fluid introductory means to introduce the fluid from the supply of fluid into the engine, the steps of: designing and constructing the engine to operate as a gas turbine engine, without introduction of the fluid, at a preferred thermal efficiency range in a predetermined compressor flow pressure ratio range and a predetermined turbine flow pressure ratio range; sensing, during engine operation, with the compressor sensing means, actual compressor operating parameters sufficient to identify the operating compressor flow pressure ratio; sensing, during engine operation, with the turbine sensing means, actual turbine operating parameters sufficient to identify the operating turbine flow pressure ratio; comparing the sensed actual operating compressor flow and turbine flow pressure ratios with the predetermined compressor flow and turbine flow pressure ratio ranges; and then introducing and modulating the fluid into the engine through the fluid introduction means downstream of the compressor inlet as required to maintain the compressor and the turbine flow pressure ratios in their respective predetermined ranges.
Claim 3
Dependent Claim
11 words
The method of claim 1 in which the fluid is steam.
Claim 4
Dependent Claim
48 words
The method of claim 2 including the additional steps, prior to introducing the fluid into the engine, of: providing a water supply; and extracting heat from the engine to convert water from the water supply to steam for introduction of the steam into the engine as the fluid.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-04-27 | 1990-10-27 | 1991-04-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-04-27 | 1994-10-27 | 1995-04-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-04-27 | 1998-10-27 | 1999-04-28 | $7700.00 | Window Closed / Lapsed |