Steam driven variable speed booster compressor for gas turbine

• US 6,003,298 A
• Filed: 10/22/1997
• Issued: 12/21/1999
• Est. Priority Date: 10/22/1997
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Horner, Michael W.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US08/955,803
• Time in Patent Office: 790 Days
• Field of Search: 60/39.161, 60/39.181, 60/39.182, 60/39.54, 60/726
• US Class Current: 60/39.182
• CPC Class Codes: F01D 17/145 by means of valves, e.g. for steam turbines valves in general F16K
• CPC Class Codes: F01K 23/10 with exhaust fluid of one cycle heating the fluid in another cycle F01K17/025 takes precedence
• CPC Class Codes: F02C 3/10 with another turbine driving an output shaft but not driving the compressor
• CPC Class Codes: F02C 3/30 Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases F02C7/141, F02C7/30, F01D21/00, F01K21/04, F23D11/10 take precedence
• CPC Class Codes: F02C 3/36 Open cycles
• CPC Class Codes: F02C 6/18 using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants using waste heat as source of energy for refrigeration plants F25B27/02; using the waste heat of a gasturbine for steam generation or in a steam cycle see F01K23/10
• CPC Class Codes: F02C 7/143 before or between the compressor stages
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F05D 2260/211 by intercooling, e.g. during a compression cycle
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A gas turbine engine that includes a steam driven variable speed booster compressor is described. In one embodiment, the engine includes a low pressure turbine and a booster compressor rotatable on a low pressure shaft. The engine further includes a high pressure compressor, a high pressure combustor, and a high pressure turbine rotatable on a high pressure (HP) shaft and forming the core engine. The output of the low pressure compressor is supplied to an intercooler, and the output of the intercooler is supplied to the high pressure compressor. The engine further includes a power turbine downstream of the high pressure turbine, and the power turbine is coupled to a generator by a shaft. The output exhaust of the power turbine is supplied to an exhaust heat boiler, and steam output by the boiler is supplied to, and drives, the low pressure turbine. Steam from the boiler may also be supplied to the high pressure combustor and to the power turbine. Since the steam is generated from the power turbine exhaust heat, the amount of steam flow can be independently varied from the gas turbine engine primary conditions, consistent of course with the gas turbine exhaust flow/temperature limitations.

Claims

1. A gas turbine engine comprising:

a low pressure turbine;

a booster compressor coupled to said low pressure turbine by a first shaft;

a high pressure compressor for receiving airflow from said booster compressor;

a high pressure turbine coupled to said high pressure compressor by a second shaft;

a combustor located intermediate said high pressure compressor and said high pressure turbine;

a power turbine downstream of said high pressure turbine;

an exhaust heat boiler coupled to receive exhaust from said power turbine, an outlet of said exhaust heat boiler coupled to an inlet of said low pressure turbine; and

a control valve for controlling flow of steam from said exhaust heat boiler to said pressure turbine, wherein a speed of said booster compressor is controllable substantially independently of a speed of said high pressure compressor.

2. An engine in accordance with claim 1 further comprising an intercooler coupled to an outlet of said low pressure compressor and to an inlet of said high pressure compressor.

3. An engine in accordance with claim 1 further comprising a generator coupled to said power turbine by an output shaft.

4. An engine in accordance with claim 1 wherein said outlet of said exhaust heat boiler is further coupled to said combustor and to said power turbine.

5. An engine in accordance with claim 1 further comprising a steam turbine, said outlet of said exhaust heat boiler coupled to an inlet of said steam turbine.

6. An engine in accordance with claim 1 wherein steam from said low pressure turbine is supplied to at least one of said combustor, said high pressure turbine, and said power turbine.

7. A gas turbine engine comprising:

a steam driven low pressure turbine;

a booster compressor coupled to said low pressure turbine by a first shaft;

a high pressure compressor for receiving airflow from said booster compressor;

a high pressure turbine coupled to said high pressure compressor by a second shaft;

a combustor located intermediate said high pressure compressor and said high pressure turbine;

an intercooler coupled to an outlet of said low pressure compressor and to an inlet of said high pressure compressor; and

a power turbine downstream of said high pressure turbine, and a generator coupled to said power turbine by an output shaft.

8. An engine in accordance with claim 7 further comprising an exhaust heat boiler coupled to receive exhaust from said power turbine, an outlet of said exhaust heat boiler coupled to an inlet of said low pressure turbine.

9. An engine in accordance with claim 8 further comprising a control valve for controlling flow of steam from said exhaust heat boiler to said low pressure turbine.

10. Arqengine in accordance with claim 8 wherein said outlet of said exhaust heat boiler is further coupled to said combustor and to said power turbine.

11. An engine in accordance with claim 8 further comprising a steam turbine, said outlet of said exhaust heat boiler coupled to an inlet of said steam turbine.

12. An engine in accordance with claim 8 wherein steam from said low pressure turbine is supplied to at least one of said combustor, said high pressure turbine, and said power turbine.

13. A gas turbine engine comprising:

a low pressure turbine;

a booster compressor coupled to said low pressure turbine by a first shaft;

a high pressure compressor for receiving airflow from said booster compressor;

a high pressure turbine coupled to said high pressure compressor by a second shaft;

a combustor located intermediate said high pressure compressor and said high pressure turbine;

a power turbine downstream of said high pressure turbine;

a generator coupled to said power turbine by an output shaft; and

an exhaust heat boiler coupled to receive exhaust from said power turbine, said exhaust heat boiler supplying steam to said low pressure turbine.

14. An engine in accordance with claim 13 further comprising a control valve for controlling flow of steam from said exhaust heat boiler to said low pressure turbine.

15. An engine in accordance with claim 13 wherein said exhaust heat boiler further supplying steam to at least one of said combustor, said high pressure turbine, and said power turbine.

16. An engine in accordance with claim 15 further comprising a control valve for controlling flow of steam from said exhaust heat boiler to said at least one of said combustor, said high pressure turbine, and said power turbine.

17. An engine in accordance with claim 13 further comprising a steam turbine, said exhaust heat boiler further supplying steam to said steam turbine.

18. An engine in accordance with claim 13 further comprising an intercooler coupled to said low pressure compressor and to said high pressure compressor.