Performance enhanced gas turbine powerplants

• US 5,490,377 A
• Filed: 01/12/1994
• Issued: 02/13/1996
• Est. Priority Date: 10/19/1993
• Status: Expired due to Fees

• Current Assignee: California Energy Commission (State of California)
• Original Assignee: California Energy Commission (State of California)
• Inventors: Janes, Clarence W.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US08/182,661
• Time in Patent Office: 762 Days
• Field of Search: 60/39.02, 60/39.12, 60/39.465, 60/39.511, 60/736, 60/728
• US Class Current: 60/39.12
• CPC Class Codes: F01D 1/00 Non-positive-displacement machines or engines, e.g. steam turbines wit working-fluid flows in opposite axial directions for balancing axial thrust F01D3/02; with other than pure rotation F01D23/00; turbines characterised by their use in special steam systems, cycles, or processes, regulating devices therefor F01K
• CPC Class Codes: F01D 1/023 the working-fluid being divided into several separate flows F01D3/02 takes precedence; several separate fluid flows being united in a single flow; the machine or engine having provision for two or more different possible fluid flow paths
• CPC Class Codes: F01D 13/00 Combinations of two or more machines or engines F01D15/00 takes precedence; combinations of two or more pumps F04; fluid gearing F16H
• CPC Class Codes: F01K 21/047 having at least one combustion gas turbine
• CPC Class Codes: F02C 1/06 using reheated exhaust gas F02C1/08 takes precedence
• CPC Class Codes: F02C 3/28 using a separate gas producer for gasifying the fuel before combustion
• CPC Class Codes: F02C 6/003 Gas-turbine plants with heaters between turbine stages
• CPC Class Codes: F02C 7/143 before or between the compressor stages
• CPC Class Codes: F02C 7/18 the medium being gaseous, e.g. air F02C7/125 takes precedence
• CPC Class Codes: F02C 7/185 Cooling means for reducing the temperature of the cooling air or gas
• CPC Class Codes: F02C 7/224 Heating fuel before feeding to the burner
• CPC Class Codes: F05D 2260/10 Particular cycles
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A gas turbine driven powerplant having one or more compressors for producing a down stream air flow, a heat exchanger positioned down stream of the compressors followed by a side stream flow coolant line, a regenerator positioned down stream of the heat exchanger and side stream coolant line, a combustor positioned down stream of the regenerator, one or more turbines positioned down stream of the combustor and mechanically coupled to the compressors, and a power turbine positioned down stream of the turbines. Combustible effluent flows through the heat exchanger and to the combustor, and air discharged from the compressors flows through the heat exchanger and to the coolant line and regenerator. Heat is transferred from the compressor discharge air to the combustible effluent, thereby producing cooling air and heating the combustible effluent. The heat exchanger can be a heat exchanger or a methane/steam reformer which produces a hydrogen-rich, low NO_x, steam diluted combustible effluent. In further embodiments, a small portion of the cool air is combined with the recuperation water in a heat recovery unit to allow vaporization of the water throughout the initial portion of the heat exchange path and form a two phased feed of water and air to the combustor. Additionally, in all embodiments a portion of the cooled compressed air can be processed by a compressor/expander for providing coolant to the turbines, compressors, and auxiliary equipment.

Claims

1. A gas turbine driven powerplant, comprising:

(a) compressor means for producing a downstream flow of air;

(b) heat exchanger means for cooling said downstream flow of air from said compressor means, said heat exchanger means positioned downstream of said compressor, said heat exchanger means including a fuel carrying coil;

(c) a regenerator positioned downstream of said heat exchanger means;

(d) cooling means for carrying a side stream of cooled air from said heat exchanger means to hot section components and/or auxiliary equipment, said cooling means positioned downstream of said heat exchanger means and upstream of said regenerator;

(e) a combustor positioned downstream of said regenerator, said combustor including a fuel inlet coupled to said fuel carrying coil of said heat exchanger means; and

(f) a turbine positioned downstream of said combustor.

2. An apparatus as recited in claim 1, further comprising steam raising means for pressure expansion and equalization of a steam/fuel mixture flowing through said fuel carrying coil of said heat exchanger means.

3. An apparatus as recited in claim 2, wherein said steam raising means comprises:

(a) a turbine, said turbine including a steam/fuel mixture inlet coupled to said heat exchanger means, said turbine including a steam/fuel mixture outlet coupled to said fuel inlet of said combustor;

(b) a compressor, said compressor including a steam/fuel mixture inlet coupled to said heat exchanger means, said compressor including a steam/fuel mixture outlet coupled to said fuel inlet of said combustor.

4. An apparatus as recited in claim 1, further comprising a power turbine positioned downstream of said turbine.

5. An apparatus as recited in claim 4, wherein said regenerator is positioned downstream of said power turbine.

6. An apparatus as recited in claim 4, wherein said cooling means provides coolant air to said turbines.

7. An apparatus as recited in claim 6, wherein said cooling means provides coolant air to said compressor.

8. An apparatus as recited in claim 5, further comprising:

(a) a methane/steam reformer positioned downstream of said power turbine, said methane/steam reformer including a fuel carrying coil disposed between said fuel carrying coil of said heat exchanger means and said fuel inlet of said combustor;

(b) a second heat exchanger, said second heat exchanger positioned downstream of said methane/steam reformer, said second heat exchanger including a fuel carrying coil coupled to said fuel carrying coil of said methane/steam reformer.

9. An apparatus as recited in claim 5, further comprising:

(a) a first methane/steam reformer positioned downstream of said power turbine, said first methane/steam reformer including a fuel carrying coil disposed between said fuel carrying coil of said heat exchanger means and said fuel inlet of said combustor;

(b) a second methane/steam reformer positioned downstream of said power turbine, said second methane/steam reformer including a fuel carrying coil;

(c) a second heat exchanger, said second heat exchanger positioned downstream of said second methane/steam reformer, said second heat exchanger including a fuel carrying coil coupled to said fuel carrying coil of said second methane/steam reformer; and

(d) a reheat combustor positioned downstream of said turbine and upstream of said power turbine, said reheat combustor including a fuel inlet coupled to said fuel carrying coil of said second methane/steam reformer.

16. An apparatus as recited in claim 1 or 10, further comprising compressor/expander means for increasing the pressure of cool air from said heat exchanger means for cooling said compressor.

17. An apparatus as recited in claim 16, further comprising condenser means for using cool air from said compressor/expander means to condense coolant vapor carrying heat from auxiliary plant equipment, and providing heated air to said combustor.

10. A chemically recuperative and thermally regenerative gas turbine driven powerplant, comprising:

(a) compressor means for producing a downstream flow of air;

(b) a methane/steam reformer positioned downstream of said compressor, said methane/steam reformer including a fuel inlet and fuel outlet, said methane/steam reformer including heat exchanger means for cooling said downstream flow of air from said compressor;

(c) a regenerator positioned downstream of said methane/steam reformer;

(d) cooling means for carrying a side stream of cooled air from said methane/steam reformer to cool hot section components and/or auxiliary equipment, said cooling means positioned downstream of said methane/steam reformer and upstream of said regenerator;

(e) a combustor positioned downstream of said regenerator, said combustor including a fuel inlet coupled to said fuel outlet of said methane/steam reformer; and

(f) a turbine positioned downstream of said combustor.

11. An apparatus as recited in claim 10, further comprising a power turbine positioned downstream of said turbine.

12. An apparatus as recited in claim 11, wherein said regenerator is positioned downstream of said power turbine.

13. An apparatus as recited in claim 11, wherein said cooling means provides coolant air to said turbines.

14. An apparatus as recited in claim 13, wherein said cooling means provides coolant air to said compressor.

15. An apparatus as recited in claim 10, further comprising:

(a) a second methane/steam reformer, said second methane/steam reformer positioned downstream of said power turbine, said second methane/steam reformer including a fuel inlet and a fuel outlet, said fuel outlet of said second methane steam reformer coupled to said fuel inlet of said combustor.

18. A gas turbine driven powerplant, comprising:

(a) compressor means for producing a downstream flow of air;

(b) heat exchanger means for cooling said downstream flow of air from said compressor means, said heat exchanger means positioned downstream of said compressor, said heat exchanger means including a fuel carrying coil;

(c) a regenerator positioned downstream of said heat exchanger means;

(d) cooling means for carrying a side stream of cooled air from said heat exchanger means to hot section components and/or auxiliary equipment, said cooling means positioned downstream of said heat exchanger means and upstream of said regenerator;

(e) a combustor positioned downstream of said regenerator, said combustor including a fuel inlet coupled to said fuel carrying coil of said heat exchanger means;

(f) a turbine positioned downstream of said combustor; and

(g) a power turbine positioned downstream of said turbine;

said cooling means providing coolant air to said turbines.

19. A chemically recuperative and thermally regenerative gas turbine driven powerplant, comprising:

(a) compressor means for producing a downstream flow of air;

(b) a methane/steam reformer positioned downstream of said compressor, said methane/steam reformer including a fuel inlet and fuel outlet;

(c) a regenerator positioned downstream of said methane/steam reformer;

(d) cooling means for carrying a side stream of cooled air from said methane/steam reformer to cool hot section components and/or auxiliary equipment, said cooling means positioned downstream of said methane/steam reformer and upstream of said regenerator;

(e) a combustor positioned downstream of said regenerator, said combustor including a fuel inlet coupled to said fuel outlet of said methane/steam reformer;

(f) a turbine positioned downstream of said combustor; and

(g) a power turbine positioned downstream of said turbine, said cooling means providing coolant air to said turbines.

20. A gas turbine driven powerplant, comprising:

(a) compressor means for producing a downstream flow of air;

(b) heat exchanger means for cooling said downstream flow of air from said compressor means, said heat exchanger means positioned downstream of said compressor means, said heat exchanger means including fuel carrying coils;

(c) a combustor positioned downstream of said heat exchanger means;

(d) a turbine positioned downstream of said combustor; and

(e) steam raising means for pressure expansion and equalization of a steam/fuel mixture flowing through said fuel carrying coils.

21. An apparatus as recited in claim 20, wherein said steam raising means comprises:

(a) a turbine, said turbine including a steam/fuel mixture inlet coupled to said heat exchanger means, said turbine including a steam/fuel mixture outlet coupled to said combustor; and

(b) a compressor, said compressor including a steam/fuel mixture inlet coupled to said heat exchanger means, said compressor including a steam/fuel mixture outlet coupled to said combustor.

22. A gas turbine driven powerplant, comprising:

(a) compressor means for producing a downstream flow of air;

(b) heat exchanger means for cooling said downstream flow of air from said compressor means, said heat exchanger means positioned downstream of said compressor means;

(c) a combustor positioned downstream of said heat exchanger means;

(d) a turbine positioned downstream of said combustor; and

(e) compressor/expander means for increasing the pressure of cool air from said heat exchanger means for cooling said compressor means.

23. A gas turbine driven powerplant, comprising:

(a) compressor means for producing a downstream flow of air;

(b) heat exchanger means for cooling said downstream flow of air from said compressor means, said heat exchanger means positioned downstream of said compressor;

(c) a combustor positioned downstream of said heat exchanger means;

(d) a turbine positioned downstream of said combustor;

(e) compressor/expander means for increasing the pressure of cool air from said heat exchanger means for cooling said compressor means; and

(f) condenser means for using cool air from said compressor/expander means to condense coolant vapor carrying heat from auxiliary plant equipment, and providing heated air to said combustor.

24. A gas turbine driven powerplant, comprising:

(a) compressor means for producing a downstream flow of air;

(b) heat exchanger means for cooling said downstream flow of air from said compressor means, said heat exchanger means positioned downstream of said compressor means;

(c) a combustor positioned downstream of said heat exchanger means;

(d) a turbine positioned downstream of said combustor; and

(e) cooled air carrying means for carrying a side stream of cooled air from said heat exchanger means to hot section components and/or auxiliary equipment, said cooled air carrying means positioned downstream of said heat exchanger means.