Variable flow compressor of a gas turbine

Patent metadata

Field	Value
Publication number	US-10036325-B2
Application number	US-201615086051-A
Country	US
Kind code	B2
Filing date	Mar 30, 2016
Priority date	Mar 30, 2016
Publication date	Jul 31, 2018
Grant date	Jul 31, 2018

Abstract

A system and medium for controlling a fuel gas compressor of a gas turbine system that compresses a gaseous fuel for consumption in a high-pressure combustor. Moreover, the compressor is configured to generate a discharge pressure for the combustor based at least in part on a load demand for the gas turbine system.

First claim

The invention claimed is:

1. A gas turbine system, comprising:
a combustor configured to burn a fuel and air mixture;
a fuel gas compressor configured to compress fuel, wherein the fuel gas compressor is configured to generate a discharge pressure for the combustor based at least in part on a load demand for the gas turbine system, and the load demand is based at least in part on a load of the gas turbine system, and the load is a generator, and the fuel gas compressor comprises a screw compressor having a slide valve configured to control a displacement volume of the fuel gas compressor; and
a controller configured to control the slide valve based at least in part on the load demand.

2. The gas turbine system of claim 1 , wherein the fuel gas compressor discharge pressure has a minimum threshold that is independent of the load demand.

3. The gas turbine system of claim 2 , wherein the minimum threshold that corresponds to a pressure differential across the fuel gas compressor that is sufficient to flow lubricant through the fuel gas compressor.

4. The gas turbine system of claim 3 , wherein oil flows to screws of the fuel gas compressor, bearings of the fuel gas compressor, seals of the fuel gas compressor, a slide valve actuator of the fuel gas compressor, or a combination thereof.

5. The gas turbine system of claim 1 , wherein the fuel gas compressor comprising:
a suction port configured to pull in fuel gas for compression; and
a recycle valve configured to return compressor discharge back to the suction port.

6. The gas turbine system of claim 5 , wherein the recycle valve is configured to make relatively quick reductions to discharge pressure of the fuel gas compressor.

7. The gas turbine system of claim 6 , wherein the slide valve is configured to adjust the displacement volume while the recycle valve is at least partially closed after the relatively quick reduction has been made.

8. The gas turbine system of claim 6 , wherein the fuel and air mixture entering the gas turbine combustor comprises ambient air and gas fuel.

9. A gas turbine system comprising:
a combustor configured to burn a fuel and air mixture;
a fuel gas compressor configured to compress gas fuel, wherein the fuel gas compressor comprises a screw compressor having a slide valve; and
a controller comprising:
a processor configured to control the fuel gas compressor; and
memory storing instructions that cause the processor to:
vary a discharge pressure from the fuel gas compressor by changing displacement volume of the fuel gas compressor using the slide valve based at least in part on load demand for the gas turbine system, wherein the load demand is based at least in part on a load of the gas turbine system and the load is a generator; and
limit the discharge pressure to a value above a minimum threshold.

10. The gas turbine system of claim 9 , wherein the minimum threshold corresponds to a pressure differential across the fuel gas compressor that is sufficient to flow lubricant through the fuel gas compressor.

11. The gas turbine system of claim 10 , wherein the fuel gas compressor comprises:
a recycle valve configured to return compressor discharge back to a suction port of the screw compressor.

12. The gas turbine system of claim 11 , wherein the instructions are configured to cause the processor to set the slide valve to an initial value at start up of the gas turbine system.

13. The gas turbine system of claim 12 , wherein the initial value comprises a smallest displacement volume selectable via the slide valve.

14. The gas turbine system of claim 12 , wherein the instructions are configured to cause the processor to:
determine whether the discharge pressure of the fuel gas compressor is above an adjustment threshold after startup has initiated; and
when the discharge pressure has surpassed the adjustment threshold, increase fuel gas compressor displacement volume using the slide valve.

15. The gas turbine system of claim 14 , wherein the instructions are configured to cause the processor to:
determine whether a setpoint for the discharge pressure has been reached by the fuel gas compressor, wherein the setpoint is at least partially based on the load demand on the gas turbine system; and
when the setpoint has been reached, decrease displacement volume of the fuel gas compressor using the slide valve at least partially close the recycle valve.

16. A non-transitory, computer-readable memory storing instructions which when executed are configured to cause a processor to:
receive an indication of a load demand for a gas turbine system, wherein the load demand is based at least in part on a load of the gas turbine system and the load is a generator;
set a discharge pressure of a compressor of the gas turbine system based at least in part on the indication by changing displacement volume of the compressor using a slide valve of the compressor based at least in part on the load demand, wherein the compressor comprises a screw compressor; and
limit the discharge pressure to a value above a pressure differential across the compressor that is sufficient to flow lubricant through the compressor.

17. The non-transitory, computer-readable medium of claim 16 , wherein the instructions are configured to cause the processor to:
receive an indication that the discharge pressure is to be increased;
increase discharge pressure toward a target pressure by:
at least partially closing a recycle valve of the compressor to reduce an amount of compressor-discharged fuel from being returned from a suction port of the compressor; and
at least partially opening the slide valve to increase displacement volume of the compressor.

18. The non-transitory, computer-readable medium of claim 17 , wherein the instructions are configured to cause the processor to:
determine whether the discharge pressure has reached the target pressure; and
level the discharge pressure near the target pressure by adjusting the recycle valve and slide valve.

19. The non-transitory, computer-readable medium of claim 17 , wherein the target pressure is based at least in part on the indication of the load demand.

20. The non-transitory, computer-readable medium of claim 16 , wherein the instructions are configured to cause the processor to:
receive an indication that the discharge pressure is to be decreased;
decrease discharge pressure toward a target pressure by:
at least partially opening a recycle valve of the compressor to increase an amount of compressor-discharged fuel being returned to a suction port of the compressor; and
at least partially closing the slide valve to decrease displacement volume of the compressor.

Assignees

• Gen Electric

Inventors

• Frey George Frederick

Classifications

• F02C3/04

  having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title

• F02C9/30

  characterised by variable fuel pump output · CPC title

• F05D2270/331

  Mechanical loads · CPC title

• F04C18/16

  with helical teeth, e.g. chevron-shaped, screw type {(for non-parallel axes of movement F04C18/48)} · CPC title

• F02C9/28 Primary

  Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title