Methods and systems for mitigating distortion of gas turbine shaft

• US 8,820,046 B2
• Filed: 09/24/2010
• Issued: 09/02/2014
• Est. Priority Date: 10/05/2009
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Ross, Steven A., Agin, Thomas E.
• Primary Examiner(s): SUNG, GERALD LUTHER
• Application Number:
  US12/890,542
• Publication Number:
  US 20110232294A1
• Time in Patent Office: 1,439 Days
• Field of Search: 60/391.3, 606/46, 606/58, 60/390.91, 607/78, 607/79, 60/392.4, 607/86, 607/87
• US Class Current: 60/39.13
• CPC Class Codes: F01D 25/34 Turning or inching gear
• CPC Class Codes: F02C 7/26 Starting; Ignition
• CPC Class Codes: F05D 2260/85 Starting
• CPC Class Codes: F05D 2270/114 by limiting mechanical stresses

Abstract

Methods and systems for mitigating distortion of a shaft of a gas turbine engine are provided. One method comprises at least one step of applying intermittent rotary power to a shaft of a gas turbine engine. The step of applying intermittent power to the shaft is performed during a period where conditions of temperature differential in the engine exist capable of distorting the shaft. The methods and systems shorten the time needed to start a gas turbine engine in such a way that bowing of a shaft is not a significant problem.

Claims

1. A system for operating a gas turbine engine:

(a) at least one sensor configured to determine at least one engine operating parameter;

(b) auxiliary rotary power supply unit;

(c) a controller coupled to the at least one sensor and to the auxiliary rotary power supply unit,

wherein the controller is configured to apply at least one pulse signal to the auxiliary rotary power supply unit for applying intermittent rotary power to a shaft of a gas turbine engine when the at least one engine operating parameter is within a preselected value,

wherein the applying intermittent rotary power includes pulsing rotary power to the shaft sufficient to cause rotation of the shaft, and

the pulsing includes applying pulses of rotary power wherein each pulse causes one or more rotations of the shaft.

2. The system according to claim 1, wherein the engine operating parameter is selected from one or more of stopped state of engine, time since engine shutdown, engine temperature parameters.

3. The system according to claim 1, wherein the at least one engine operating parameter comprises temperature differential in the engine.

4. The system according to claim 1, wherein the at least one engine operating parameter comprises time since engine shutdown.

5. The system according to claim 1, wherein the controller is configured to send an abort signal to the auxiliary rotary power supply unit when a safety condition is present.

6. The system according to claim 5, wherein the auxiliary rotary power supply unit is configured to apply a braking torque to the shaft when the safety condition is present.

7. The system according to claim 1, further comprising a rotation sensor for detecting rotary motion of the shaft and the controller is further coupled to the rotation sensor.

8. The system according to claim 7, wherein the controller is configured to send a remove power signal to the auxiliary rotary power supply unit at a time when rotation is sensed.