IP Library Granted Patent US 8,505,364
Granted Patent B2
US 8,505,364 · App. 13/289,680 · Granted Aug 13, 2013

Systems and methods for use in monitoring operation of a rotating component

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,505,364
App. No.
13/289,680
Granted
Aug 13, 2013
Kind
B2
Abstract

A system for use in monitoring operation of a rotor assembly is provided. The system includes a plurality of clearance sensors including at least a first clearance sensor configured to measure a distance between the first sensor and a surface of a lockwire tab, and a monitoring unit coupled to the plurality of clearance sensors, the monitoring unit configured to receive measurements from the plurality of clearance sensors, and determine whether a crack exists in the rotor assembly based on the received measurements.

Claims (29)

1. A system for use in monitoring operation of a rotor assembly, said system comprising:

a plurality of clearance sensors comprising at least a first clearance sensor configured to measure a distance between said first sensor and a surface of a lockwire tab; and

a monitoring unit coupled to said plurality of clearance sensors, said monitoring unit configured to:

receive measurements from said plurality of clearance sensors; and

determine whether a crack exists in the rotor assembly based on the received measurements.

2. A system in accordance with claim 1 , wherein said first sensor comprises a sensor positioned to measure a distance between said first sensor and a surface of the lockwire tab that is substantially parallel to a longitudinal axis of the rotor assembly.

3. A system in accordance with claim 1 , wherein said first sensor comprises a sensor positioned to measure a distance between said sensor and a surface of the lockwire tab that is substantially perpendicular to a longitudinal axis of the rotor assembly.

4. A system in accordance with claim 1 , wherein said plurality of clearance sensors further comprises at least a second sensor positioned to measure a distance between said second sensor and a surface of a bucket coupled to the rotor assembly.

5. A system in accordance with claim 4 , wherein said second sensor comprises a sensor positioned to measure a distance between said second sensor and a tip of the bucket adjacent to a leading edge of the bucket.

6. A system in accordance with claim 4 , wherein said second sensor comprises a sensor positioned to measure a distance between said second sensor and a tip of the bucket adjacent to a trailing edge of the bucket.

7. A system in accordance with claim 1 , wherein said monitoring unit is further configured to compare measurements from at least one of said plurality of clearance sensors to determine a location of a crack in the rotor assembly.

8. A system in accordance with claim 1 , wherein said monitoring unit is configured to generate an alert when a crack is detected.

9. A monitoring unit for use in monitoring operation of a rotor assembly, said monitoring unit comprising:

a memory device configured to store measurements received from a plurality of clearance sensors that include at least a first sensor configured to measure a distance between the first sensor and a surface of a lockwire tab; and

a processing device coupled to said memory device and configured to determine whether a crack exists in the rotor assembly based on the stored measurements.

10. A monitoring unit in accordance with claim 9 , wherein said memory device is configured to store measurements from a first sensor positioned to measure a distance between the first sensor and a surface of the lockwire tab that is substantially parallel to a longitudinal axis of the rotor assembly.

11. A monitoring unit in accordance with claim 9 , wherein said memory device is configured to store measurements from a first sensor positioned to measure a distance between the first sensor and a surface of the lockwire tab that is substantially perpendicular to a longitudinal axis of the rotor assembly.

12. A monitoring unit in accordance with claim 9 , wherein said memory device is configured to store measurements from a second sensor positioned to measure a distance between the second sensor and a surface of a bucket coupled to the rotor assembly.

13. A monitoring unit in accordance with claim 12 , wherein said memory device is configured to store measurements indicative of a distance between the second sensor and a tip of the bucket adjacent to a leading edge of the bucket.

14. A monitoring unit in accordance with claim 12 , wherein said memory device is configured to store measurements indicative of a distance between the second sensor and a tip of the bucket adjacent to a trailing edge of the bucket.

15. A monitoring unit in accordance with claim 9 , wherein said processing device is further configured to compare measurements from at least one of the plurality of clearance sensors to determine a location of a crack in the rotor assembly.

16. A monitoring unit in accordance with claim 9 , wherein said processing device is configured to generate an alert when a crack is detected.

17. A method for monitoring operation of a rotor assembly, said method comprising:

acquiring, from at least one clearance sensor, measurements indicative of the distance between the at least one clearance sensor and a component of the rotor assembly, wherein the at least one clearance sensor includes a first sensor configured to measure a distance between the first sensor and a surface of a lockwire tab;

transmitting the acquired measurements to a monitoring unit; and

determining, using the monitoring unit, whether a crack exists in the rotor assembly based on the received measurements.

18. A method in accordance with claim 17 , wherein acquiring measurements comprises acquiring a measurement indicative of a distance between the first sensor and a surface of a lockwire tab that is substantially parallel to a longitudinal axis of the rotor assembly.

19. A method in accordance with claim 17 , wherein acquiring measurements comprises acquiring a measurement indicative of a distance between the first sensor and a surface of a lockwire tab that is substantially perpendicular to a longitudinal axis of the rotor assembly.

20. A method in accordance with claim 17 , further comprising comparing, using the monitoring device, measurements from at least one clearance sensors to determine a location of a crack.

Assignments (3)
CHANGE OF NAME Recorded Feb 14, 2023
From: BAKER HUGHES, A GE COMPANY, LLC
To: BAKER HUGHES, A GE COMPANY, LLC
Reel/Frame 062748/0526 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 26, 2020
From: GENERAL ELECTRIC COMPANY
To: BAKER HUGHES, A GE COMPANY, LLC
Reel/Frame 051698/0346 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 4, 2011
From: BATZINGER, THOMAS JAMES; BADAMI, VIVEK VENUGOPAL; LU, WANGMING; HOYTE, SCOTT MORDIN; GODBOLE, MANDAR DIWAKAR; BABU, RAVI YOGANATHA; BHATTACHARYA, ANINDA; KITTLESON, JACOB JOHN
To: GENERAL ELECTRIC COMPANY
Reel/Frame 027179/0033 →