Turbine speed control system and method

• US 7,194,863 B2
• Filed: 09/01/2004
• Issued: 03/27/2007
• Est. Priority Date: 09/01/2004
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Ganev, Evgeni, Koerner, Mike S., Liu, Chung Y.
• Primary Examiner(s): Casaregola; L. J.
• Application Number:
  US10/931,694
• Publication Number:
  US 20060042262A1
• Time in Patent Office: 937 Days
• Field of Search: 60/392.5, 60/392.81, 607/73, 137/599.05, 137/599.06, 137/599.07, 415/38, 415/40
• US Class Current: 60/773
• CPC Class Codes: F02C 9/28 Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed F02C9/30 - F02C9/38, F02C9/44 take precedence
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10T 137/87314 Electromagnetic or electric control [e.g., digital control, bistable electro control, etc.]

Abstract

One embodiment of the invention provides a turbine control system that adjusts the control thresholds of two-position valves, which provide propellant to the turbine, based on turbine load so as to compensate for increased turbine speed overshoot at low load and the increased turbine speed undershoot at high load. These two-position on-off modulated valves are used in a bang-bang (fully open or fully closed) regulation scheme to eliminate or minimize speed droop by using variable speed bounds implemented as a function of load.

Claims

1. A system comprising:

a turbine generator;

one or more two-position valves to provide one or more propellants to the turbine generator; and

a controller coupled to the one or more two-position valves, the controller configured to

determine an operating speed of the turbine generator,

compare the operating speed to a reference speed,

if the operating speed is greater than the reference speed then the one or more two-position valves are fully closed to reduce the speed of the turbine generator,

if the operating speed is less than the reference speed then the one or more two-position valves are fully opened to increase the speed of the turbine generator,

wherein the reference speed varies as a function of load on the turbine generator to decrease speed droop at increased loads.

2. The system of claim 1 wherein the reference speed limit includes an upper bound speed threshold and a lower bound speed threshold, if the operating speed is above the upper bound speed threshold then the one or more two-position valves are fully closed, and if the operating speed is below the lower bound speed threshold then the one or more two-position valves are fully opened.

3. The system of claim 2 wherein the upper bound speed threshold and lower bound speed threshold are adjusted based on the load on the turbine generator.

4. The system of claim 1 wherein the one or more propellants include hydrogen and oxygen.

5. The system of claim 1 further comprising:

a first two-position valve to provide hydrogen to the turbine generator; and

a second two-position valve to provide oxygen to the turbine generator,

wherein, if the operating speed is greater than an upper limit speed then the first two-position valve is fully opened before the second two-position valve is opened, and

if the operating speed is less than a lower limit speed then the second two-position valve is fully closed before the first two-position valve is closed.

6. The system of claim 5 wherein the upper limit speed is greater than the reference speed and the lower limit speed is less than the reference speed.

7. The system of claim 5 wherein the time interval between opening the first two-position valve and opening the second two-position valve is increased to decrease the temperature of the turbine generator.

8. The system of claim 1 wherein the load on the turbine generator is estimated from the delivered DC power and the average efficiencies of its components.

9. A method for controlling turbine speed comprising:

determining the operating speed of the turbine;

comparing the operating speed to an upper reference speed and a lower reference speed;

increasing the speed of the turbine if the operating speed is less than the lower reference speed;

decreasing the speed of the turbine if the operating speed is greater that the upper reference speed;

determining the load on the turbine; and

adjusting the upper reference speed and lower reference speed as a function of the load on the turbine.

10. The method of claim 9 further comprising:

fully opening one or more two-position valves if increasing the speed of the turbine; and

fully closing one or more two-position valves if decreasing the speed of the turbine.

11. The method of claim 9 further comprising:

estimating the delivered DC power by the turbine and the average efficiencies of the turbine components to determine the load on the turbine.

12. The method of claim 9 wherein the one or more propellants include hydrogen and oxygen.

13. The method of claim 12 wherein a first two-position valve to provide hydrogen to the turbine generator and a second two-position valve to provide oxygen to the turbine generator, and further comprising:

fully opening the first two-position valve before opening the second two-position valve if the operating speed is greater than an upper reference speed; and

closing the second two-position valve before closing the first two-position valve if the operating speed is less than a lower reference speed.

14. The method of claim 13 wherein the time difference between opening the first two-position valve and opening the second two-position valve is increased to decrease the temperature of the turbine generator.

15. A turbine comprising:

a power generator;

one or more two-position valves provide a propellant to the power generator;

a controller configured to

determine an operating speed for the turbine,

compare the operating speed to an upper reference speed and a lower reference speed,

increase the speed of the turbine if the operating speed is less than the lower reference speed,

decrease the speed of the turbine if the operating speed is greater that the upper reference speed,

determine the load on the turbine, and

adjust the upper reference speed and lower reference speed as a function of the load on the turbine to decrease speed droop at increased loads.

16. The turbine of claim 15 the controller is further configured to

fully open one or more two-position valves if increasing the speed of the turbine, and

fully close one or more two-position valves if decreasing the speed of the turbine.

17. The turbine of claim 15 further comprising:

a first two-position valve to provide hydrogen to the power generator; and

a second two-position valve to provide oxygen to the power generator,

wherein the controller is further configured to

fully open the first two-position valve before opening the second two-position valve if the operating speed is greater than an upper reference speed, and

fully close the second two-position valve before closing the first two-position valve if the operating speed is less than a lower reference speed.

18. The turbine of claim 15 wherein the load on the turbine generator is estimated from the power generator.

19. The turbine of claim 15 wherein the upper reference speed and the lower reference speed are adjusted based on the load on the turbine.

20. The turbine of claim 15 wherein the propellant includes hydrogen and oxygen.