System for determining target misalignment in turbine shaft and related method

• US 8,910,531 B1
• Filed: 07/03/2013
• Issued: 12/16/2014
• Est. Priority Date: 07/03/2013
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Sue, Peter Ping-Liang, Farr, Lawrence Brown II, Kretschmar, Andrea Booher
• Primary Examiner(s): Caputo, Lisa
• Assistant Examiner(s): WILLIAMS, JAMEL E
• Application Number:
  US13/934,599
• Publication Number:
  US 20150010386A1
• Time in Patent Office: 531 Days
• Field of Search: 738/620.8, 738/620.41
• US Class Current: 73/862.08
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: F01D 21/045 special arrangements in stators or in rotors dealing with breaking-off of part of rotor
• CPC Class Codes: G01B 11/272 using photoelectric detection means
• CPC Class Codes: G01B 21/24 for testing alignment of axes
• CPC Class Codes: G01M 15/14 Testing gas-turbine engines or jet-propulsion engines
• CPC Class Codes: Y02E 20/16 Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Abstract

Systems and devices configured to determine misalignment of targets of a rotating shaft by monitoring axial and radial aspects of targets and the shaft. In one embodiment, a target monitoring system includes a first horizontal probe communicatively connected to at least one first horizontal target connected to the shaft, and a first axial probe located adjacent to the first horizontal probe and communicatively connected to the first horizontal target. The system also includes a second horizontal probe communicatively connected to at least one second horizontal target connected to the shaft, and a second axial probe located adjacent to the second horizontal probe and communicatively connected to the second horizontal target. The system may further include an end probe disposed proximate a first end of the shaft for monitoring axial movement of the shaft, and a computing device communicatively connected to the end probe and each horizontal and axial probe.

Claims

1. A target monitoring system comprising:

a first horizontal probe located radially outboard of a shaft and communicatively connected to at least one first horizontal target connected to the shaft, the at least one first horizontal target disposed proximate a first end of the shaft;

a first axial probe located axially adjacent to the first horizontal probe and communicatively connected to the at least one first horizontal target;

a second horizontal probe located radially outboard of the shaft communicatively connected to at least one second horizontal target connected to the shaft, the at least one second horizontal target disposed proximate a second end of the shaft;

a second axial probe located axially adjacent to the second horizontal probe and communicatively connected to the at least one second horizontal target;

an end probe disposed proximate the first end of the shaft, the end probe configured to monitor axial movement of the shaft; and

a computing device communicatively connected to the end probe and each of the first horizontal probe, the first axial probe, the second horizontal probe and the second axial probe,

wherein the computing device is configured to;

determine a first gradient for the at least one first horizontal target based on a displacement between the first horizontal probe and the at least one first horizontal target and the first axial probe and the at least one first horizontal target; and

determine a second gradient for the at least one second horizontal target based on a displacement between the second horizontal probe and the at least one second horizontal target and the second axial probe and the at least one second horizontal target.

2. The target monitoring system of claim 1, wherein the end probe includes at least one of:

a Bentley Nevada probe, a clearance probe and a magnetic pick-up probe.

3. The target monitoring system of claim 1, wherein at least one of the first horizontal probe, the first axial probe, the second horizontal probe, and the second axial probe include an optical probe.

4. The target monitoring system of claim 1, wherein the first horizontal probe and the first axial probe are located a predetermined distance apart in the axial direction relative to the shaft.

5. The target monitoring system of claim 1, wherein the computing device is configured to determine misalignment between the at least one first horizontal target and the at least one second horizontal target based on the axial movement of the shaft and the first gradient and the second gradient of the at least one first horizontal target and the at least one second horizontal target.

6. The target monitoring system of claim 1, further comprising a plurality of targets disposed circumferentially about the shaft and communicatively connected to at least one of:

the first horizontal probe, the first axial probe, the second horizontal probe, and the second axial probe.

7. The target monitoring system of claim 6, further comprising a plurality of probes communicatively connected to the plurality of targets and the computing device, the computing device further configured to monitor the plurality of targets during rotation of the shaft via the plurality of probes,

wherein the computing device is configured to determine torsional displacement of the shaft based on the monitoring of the plurality of targets, and

wherein the computing device is configured to factor axial movement of the shaft in the torsional displacement determination.

8. A method comprising:

determining a first primary displacement between a first horizontal probe and at least one first target on a shaft, the at least one first target located proximate a first end of the shaft;

determining a second primary displacement between a first axial probe and the at least one first target;

calculating a first gradient of the at least one first target based on the first primary displacement and the second primary displacement;

monitoring axial movement of the shaft via an end probe; and

determining an amount of false twisting of the shaft at load condition based on;

a difference between the first gradient and a calculated second gradient; and

the axial movement of the shaft.

9. The method of claim 8, further comprising:

determining a first secondary displacement between a second horizontal probe and at least one second target on the shaft, the at least one second target located proximate a second end of the shaft;

determining a second secondary displacement between a second axial probe and the at least one second target; and

calculating the second gradient of the second target based on the first secondary displacement and the second secondary displacement.

10. The method of claim 8, wherein the shaft is at a no load condition during the determining of the first displacement and the determining of the second displacement.

11. The method of claim 8, wherein the shaft is at a load condition during the monitoring of the axial movement.

12. The method of claim 8, wherein the end probe includes at least one of:

a Bentley Nevada probe, a clearance probe and a magnetic pick-up probe.

13. The method of claim 8, wherein the first horizontal probe and the first axial probe are located a predetermined distance apart in the axial direction relative to the shaft.

14. The method of claim 8, wherein at least one of the first horizontal probe, the first axial probe, the second horizontal probe, and the second axial probe include an optical probe.

15. The method of claim 8, further comprising:

monitoring via a computing device a plurality of probes communicatively connected to a plurality of targets disposed on the shaft, the computing device configured to monitor the plurality of targets during rotation of the shaft via the plurality of probes,

wherein the computing device is configured to determine torsional displacement of the shaft based on the monitoring of the plurality of targets, and

wherein the computing device is configured to factor axial movement of the shaft in the torsional displacement determination.

16. A turbine comprising:

a stator;

a working fluid passage substantially surrounded by the stator; and

a shaft configured radially inboard of the stator and in the working fluid passage; and

a target monitoring system communicatively connected to the shaft and configured to monitor displacement of the shaft during operation of the turbine, the target monitoring system including;

a first horizontal probe located radially outboard of the shaft and communicatively connected to at least one first horizontal target connected to the shaft, the at least one first horizontal target disposed proximate a first end of the shaft;

a first axial probe located axially adjacent to the first horizontal probe and communicatively connected to the at least one first horizontal target;

a second horizontal probe located radially outboard of the shaft communicatively connected to at least one second horizontal target connected to the shaft, the at least one second horizontal target disposed proximate a second end of the shaft;

a second axial probe located axially adjacent to the second horizontal probe and communicatively connected to the at least one second horizontal target;

an end probe disposed proximate the first end of the shaft, the end probe configured to monitor axial movement of the shaft; and

a computing device communicatively connected to the end probe and each of the first horizontal probe, the first axial probe, the second horizontal probe and the second axial probe,

wherein the computing device is configured to;

determine a first gradient for the at least one first horizontal target based on a displacement between the first horizontal probe and the at least one first horizontal target and the first axial probe and the at least one first horizontal target; and

determine a second gradient for the at least one second horizontal target based on a displacement between the second horizontal probe and the at least one second horizontal target and the second axial probe and the at least one second horizontal target.

17. The turbine of claim 16, wherein the end probe includes at least one of:

a Bentley Nevada probe, a clearance probe and a magnetic pick-up probe.

18. The turbine of claim 16, wherein at least one of the first horizontal probe, the first axial probe, the second horizontal probe, and the second axial probe include an optical probe.

19. The turbine of claim 16, wherein the first horizontal probe and the first axial probe are located a predetermined distance apart in the axial direction relative to the shaft.

20. The turbine of claim 16, wherein the computing device is configured to determine misalignment between the at least one first horizontal target and the at least one second horizontal target based on the axial movement of the shaft and the first gradient and the second gradient of the at least one first horizontal target and the at least one second horizontal target.