Permanent magnet rotor crack detection

• US 8,095,324 B2
• Filed: 06/26/2008
• Issued: 01/10/2012
• Est. Priority Date: 06/26/2008
• Status: Active Grant

• Current Assignee: Pratt & Whitney Canada Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Pratt & Whitney Canada Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Dooley, Kevin A.
• Primary Examiner(s): BHAT, ADITYA S
• Application Number:
  US12/146,606
• Publication Number:
  US 20090322373A1
• Time in Patent Office: 1,293 Days
• Field of Search: 702/35
• US Class Current: 702/35
• CPC Class Codes: G01N 27/82 for investigating the presence of flaws
• CPC Class Codes: G01R 31/343 in operation

Abstract

A method and apparatus for permanent magnetic (PM) rotor crack detection includes a sensor which monitors magnetic flux distribution of the PM rotor and identifies the presence of a crack in the PM rotor when a magnetic flux distribution change or anomaly is detected.

Claims

1. A method for detecting cracks in a permanent magnetic rotor of an electric motor/generator, comprising:

a) providing an apparatus for sensing a magnetic flux field in motion;

b) using said apparatus to sense a magnetic flux distribution of a magnetic flux field of the permanent magnetic rotor when the magnetic flux field rotates together with the rotor;

c) using the apparatus to monitor the magnetic flux distribution of the magnetic flux field of the permanent magnetic rotor;

d) detecting an anomaly in the magnetic flux distribution using the apparatus, the anomaly associated with a location on the permanent magnetic rotor;

e) identifying a crack location on the permanent magnetic rotor associated with said rotor location.

2. The method as defined in claim 1 wherein the crack location includes at least one of a rotor circumferential position and a rotor axial position of said crack.

3. The method as defined in claim 1 comprising determining an axial position of the anomaly on the rotor by confining said step of detecting to a selected first axial section of the rotor and then performing said step of detecting on other axial sections of the rotor until an anomaly is detected, the axial section within which the anomaly was detected being associated with a rotor axial position of the crack.

4. The method as defined in claim 3 wherein the selected axial sections are polled serially successively by a magnetic flux distribution single sensor.

5. The method as defined in claim 3 wherein the apparatus includes a sensor positioned in a second location adjacent the permanent magnetic rotor, and then repeating steps (c) and (d), the second location being axially adjacent the first location with respect to an axial length of the permanent magnetic rotor.

6. The method as defined in claim 5 comprising repeating steps (b), (c) and (d) until discrete locations in which the sensor has been positioned extend across the axial length of the permanent magnetic rotor.

7. The method as defined in claim 1 wherein the anomaly is detected by comparing a measured magnetic flux distribution with a reference magnetic flux distribution.

8. The method as defined in claim 7 wherein the reference magnetic flux distribution is a previously recorded measurement associated with a crack-free rotor.

9. The method as defined in claim 1 further comprising acquiring rotor position information and using said information to determine a circumferential position of the anomaly on the rotor.

10. The method as defined in claim 9 wherein the rotor position information is obtained by providing a marker on the rotor at a known circumferential location, detecting the marker on successive rotor revolutions, and comparing information on the marker position and crack anomaly to determine the circumferential position of the crack on the rotor.

11. The method as defined in claim 10 wherein detecting the marker is achieved by using the apparatus to sense a pulse signal associated with a known magnetic marker anomaly associated with the marker of the permanent magnetic rotor.

12. The method as defined in claim 1 wherein the step of detecting an anomaly is achieved by placing an electrically conductive wire adjacent permanent magnets of the rotor, the wire included in an electric circuit of the apparatus adapted to sense electricity in the circuit.

13. The method as defined in claim 1 wherein the step of detecting the anomaly is achieved by monitoring an output of a sensor of the apparatus, the sensor placed adjacent permanent magnets of the rotor, the sensor selected from the group consisting of a Hall Effect device and a Giant Magnetoreisistance device.

14. The method as defined in claim 1 comprising repeating the four steps over time to obtain crack trending information.

15. The method as defined in claim 14 further comprising providing the crack trend information to at least one of a machine operator and a machine maintenance personnel.

16. The method as defined in claim 1 further comprising the step of setting a warning upon detection of a crack.

17. A method for detecting cracks in a permanent magnetic rotor of an electric motor/generator, comprising:

a) providing an apparatus including a wire loop for sensing a magnetic flux field in motion;

b) positioning the wire loop in a selected location adjacent the permanent magnetic rotor, the wire loop being connected to an electric circuit of the apparatus for sensing a magnetic flux distribution of a magnetic flux field of the permanent magnetic rotor when the magnetic flux field rotates together with the rotor;

c) monitoring the magnetic flux distribution of the magnetic flux field of the permanent magnetic rotor using the wire loop of the apparatus in said location during a rotor operation; and

d) identifying the presence of a crack in the permanent magnetic rotor when an unknown magnetic flux distribution anomaly of the rotor is detected.

18. The method as defined in claim 17 wherein an electric signal associated with an instant rotation cycle of the permanent magnetic rotor is compared with a recorded electric signal associated with a previous rotation cycle of the permanent magnetic rotor.

19. An electric machine system comprising:

a permanent magnetic rotor rotatably mounted adjacent a stator;

means for detecting a crack in the permanent magnetic rotor during rotation, said means using a measured magnetic flux distribution of a magnetic flux field of the permanent magnetic rotor as the magnetic flux field rotates together with the rotor during normal operation of said electric machine system; and

a computer system communicating with said means for recording information associated with a detected crack in the permanent magnetic rotor.

20. The electric machine system as defined in claim 19, wherein the means includes a sensor positioned in an air gap between the permanent magnetic rotor and a surface of a stationary housing of the electric machine system.