Overspeed detection techniques for gas turbine engine

• US 6,321,525 B1
• Filed: 02/03/2000
• Issued: 11/27/2001
• Est. Priority Date: 02/03/2000
• Status: Expired due to Term

• Current Assignee: Rolls-Royce Corporation (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce Corporation (Rolls-Royce Holdings Plc)
• Inventors: Rogers, David Mark
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US09/497,558
• Time in Patent Office: 663 Days
• Field of Search: 60/390.3, 60/390.91, 60/392.81
• US Class Current: 60/773
• CPC Class Codes: F01D 17/06 responsive to speed
• 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: F05D 2270/02 to control rotational speed (n)
• CPC Class Codes: F05D 2270/021 to prevent overspeed
• CPC Class Codes: F05D 2270/042 by keeping it below damagingly high values
• CPC Class Codes: G05B 23/0235 based on a comparison with predetermined threshold or range, e.g. "classical methods", carried out during normal operation; threshold adaptation or choice; when or how to compare with the threshold

Abstract

Unique systems and methods are disclosed to detect and remediate an overspeed condition of a gas turbine engine. Such techniques include sensing rotational speed of a rotating member of a gas turbine engine and providing a first speed threshold that varies with rotational acceleration of this member over a predefined range. An overspeed condition of the gas turbine engine is detected if the rotational speed exceeds this first speed threshold and a second speed threshold. This second speed threshold is greater than or equal to the first speed threshold when the overspeed condition is detected. In response to the overspeed detection, a fuel valve may be actuated to adjust fuel flow to the engine. In one embodiment, an analog circuit compares the first and second speed thresholds to the rotational speed and controls current flow through an actuator for an overspeed fuel valve associated with the engine.

Claims

1. A method, comprising:

sensing rotational speed of a rotating member of a gas turbine engine;

providing a first speed threshold that varies with rotational acceleration of the rotating member over a range; and

detecting an overspeed condition of the gas turbine engine if the rotational speed exceeds the first speed threshold and a second speed threshold, the second speed threshold being greater than or equal to the first speed threshold when the overspeed condition is detected.

2. The method of claim 1, further comprising actuating a fuel valve in response to said detecting.

3. The method of claim 1, wherein the second speed threshold is fixed and the first speed threshold decreases as the rotational acceleration increases.

4. The method of claim 1, wherein said detecting includes activating an electromagnetic acuator for a fuel valve with a first drive circuit and a second drive circuit, one of the first and second drive circuits sourcing electric current to the actuator and another of the first and second drive circuits sinking current from the actuator.

5. The method of claim 4, wherein the first drive circuit includes a first comparator to compare the rotational speed and the first speed threshold and the second drive circuit includes a second comparator to compare the rotational speed and the second speed threshold.

6. The method of claim 1, wherein the second speed threshold is greater than a lower extreme of the range for the first speed threshold.

7. A method, comprising:

determining rotational speed of a rotating member of a gas turbine engine; and

establishing an overspeed condition of the gas turbine engine if the rotational speed exceeds a first speed threshold and a second speed threshold, the first speed threshold varying relative to the second speed threshold in accordance with rate of change of the rotational speed.

8. The method of claim 7, further comprising actuating a fuel valve in response to the overspeed condition.

9. The method of claim 7, further comprising activating an electromagnetic acuator for a fuel valve with a first drive circuit and a second drive circuit in response to the overspeed condition, one of the first and second drive circuits sourcing electric current to the actuator and another of the first and second drive circuits sinking current from the actuator.

10. The method of claim 9, wherein the first drive circuit includes a first comparator to compare the rotational speed and the first speed threshold and the second drive circuit includes a second comparator to compare the rotational speed and the second speed threshold.

11. The method of claim 7, further comprising selecting the second speed threshold based on unexpected loss of engine load and the first speed threshold based on expected engine transient performance.

12. The method of claim 11, wherein the second speed threshold is fixed, wherein the first speed threshold decreases with increasing rotational acceleration of the rotating member.

13. An apparatus, comprising:

a gas turbine engine with a rotatable member;

a sensor to provide a first signal corresponding to rotational speed of said rotatable member;

a control responsive to said first signal to detect an overspeed condition of said gas turbine engine if the rotational speed exceeds a first speed threshold and a second speed threshold, said control being operable to determine the first speed threshold as a function of rotational acceleration of the rotatable member, the first speed threshold varying relative to the second speed threshold in accordance with the rotational acceleration; and

an actuator responsive to said control to reduce the rotational speed when the overspeed condition is detected.

14. The apparatus of claim 13, further comprising a fuel valve responsive to activation of said actuator.

15. The apparatus of claim 13, wherein said control includes an analog circuit comprising:

a first comparator operable to generate a second signal if the rotational speed exceeds the first speed threshold; and

a second comparator operable to generate a third signal if the rotational speed exceeds the second speed threshold.

16. The apparatus of claim 15, wherein said analog circuit is operable to provide electric power to said actuator in response said second and third signals, one of said second and third signals being operable to source electric current to said actuator and another of said second and third signals being operable to sink the electric current from said actuator when the rotational speed exceeds the first and second speed thresholds.

17. The apparatus of claim 13, wherein said control includes a first drive circuit and a second drive circuit, one of said first and second drive circuits sourcing electric current to said actuator and another of said first and second drive circuits sinking the electric current from said actuator when rotational speed exceeds the first and second speed thresholds.

18. The apparatus of claim 17, wherein said first drive circuit includes a first comparator responsive to the rotational speed and the first speed threshold to generate a first drive signal when the rotational speed exceeds the first threshold and said second drive circuit includes a second comparator responsive to the rotational speed and the second speed threshold to generate a second drive signal when the rotational speed exceeds the second threshold, the electric current being provided to said actuator when said first and second drive signals are contemporaneously generated.

19. The apparatus of claim 18, further comprising a differentiation circuit to determine the rotational acceleration from the rotational speed.

20. The apparatus of claim 19, further comprising a selection circuit to determine said first speed threshold based on the acceleration.

21. The apparatus of claim 13, wherein said control includes means for comparing the rotational speed to the first and second speed thresholds, means for driving said actuator, means for determining the rotational acceleration from the rotational speed, and means for selecting the first speed threshold from a predetermined range based on the rotational acceleration.