Multi-plane flexible rotor balancing

• US 20070090701A1
• Filed: 10/25/2005
• Published: 04/26/2007
• Est. Priority Date: 10/25/2005
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Stout, David, Down, Edward, Waddell, Simon
• Granted Patent: US 7,342,331 B2
• Time in Patent Office: Days
• US Class Current: 310/51
• CPC Class Codes: H02K 2205/12 Machines characterised by means for reducing windage losses or windage noise
• CPC Class Codes: H02K 3/527 applicable to rotors only
• CPC Class Codes: H02K 7/04 Balancing means

Abstract

A rotor balancing system is provided that includes a rotor core, a plurality of core channels, a support wedge, a wedge channel, and balance masses. The rotor core includes an annular section, a first pole, and a second pole. The first and second poles each extend radially outwardly from the annular section and form an interpole region therebetween. The plurality of core channels are formed in the rotor core annular section and extend axially through the rotor core annular section. The support wedge is disposed in the interpole region. The wedge channel is formed in the support wedge and extends therethrough. One or more balance masses are selectively disposed in one or more of the core channels and the wedge channel, and each balance mass is disposed at a predetermined axial location to thereby correct rotor imbalance.

Claims

1. A rotor balancing system, comprising:

a rotor core including an annular section, a first pole, and a second pole, the first and second poles each extending radially outwardly from the annular section and forming an interpole region therebetween;

a plurality of core channels formed in the rotor core annular section and extending axially through the rotor core annular section;

a support wedge disposed in the interpole region;

a wedge channel formed in the support wedge and extending therethrough; and

one or more balance masses selectively disposed in one or more of the core channels and the wedge channel, each balance mass disposed at a predetermined axial location to thereby correct rotor imbalance.

2. The system of claim 1, wherein the plurality of core channels is formed in the rotor core annular section proximate the shaft.

3. The system of claim 1, wherein the support wedge is a trapezoidally shaped rod that includes a bottom surface that contacts the rotor core annular section.

4. The system of claim 1, wherein the support wedge is a lower support wedge and the system further comprises an upper support wedge disposed in the interpole region over the lower support wedge.

5. The system of claim 4, wherein the upper support wedge includes a bottom wall, a top wall, and side walls extending therebetween.

6. The system of claim 5, further comprising a plurality of upper wedge channels extending through the upper support wedge top wall.

7. The system of claim 5, wherein at least one of the core channel and the wedge channels has threaded walls.

8. A generator rotor, comprising:

a shaft configured to rotate about an axis;

a rotor core coupled to the shaft and including an annular section, a first pole, and a second pole, the first and second poles each extending radially outwardly from the annular section and forming an interpole region therebetween;

a lower support wedge disposed in the interpole region and having a side in contact with the rotor core;

a upper support wedge disposed in the interpole region over the lower support wedge having a bottom wall, a top wall, and side walls therebetween;

a plurality of channels formed in and extending through the rotor core annular section, the lower support wedge, and the upper support wedge, each channel disposed at a different radial location relative to the axis; and

one or more balance masses selectively disposed in one or more of the channels, each balance mass disposed at a predetermined axial location to thereby correct rotor imbalance.

9. The generator rotor of claim 8, wherein at least one of the channels is formed in the upper support wedge top wall.

10. The generator rotor of claim 8, wherein at least one of the channels is formed in the rotor core annular section proximate the shaft.

11. The generator rotor of claim 8, wherein the at least one of the channels extends axially through one of the rotor core first and second poles.

12. The generator rotor of claim 8, wherein plurality of channels are substantially parallel to the axis.

13. The generator rotor of claim 8, wherein at least one of the channels has threaded walls.

14. A generator, comprising:

a stator;

a rotor rotationally mounted at least partially within the stator, the rotor including;

a shaft configured to rotate about an axis;

a rotor core coupled to the shaft and including an annular section, a first pole, and a second pole, the first and second poles each extending radially outwardly and forming an interpole region therebetween;

a lower support wedge disposed in the interpole region and having a side in contact with the rotor core;

a upper support wedge disposed in the interpole region over the lower support wedge having a bottom wall, a top wall, and side walls therebetween;

a plurality of channels formed in the rotor core annular section, the lower support wedge, and the upper support wedge, each channel disposed at a different radial location relative to the axis; and

one or more balance masses selectively disposed in one or more of the channels, each balance mass disposed at a predetermined axial location to thereby correct rotor imbalance.

15. The generator of claim 14, further comprising a first and a second coil disposed around the first and the second poles, respectively.

16. The generator of claim 14, further comprising an axial pole channel formed in one of the first and the second poles.

17. The generator of claim 14, wherein at least one of the channels is formed in the upper support wedge top wall.

18. The generator of claim 14, wherein at least one of the channels is formed in the rotor core annular section proximate the shaft.

19. The generator of claim 14, wherein the plurality of channels are substantially parallel to the axis.