ELECTRIC MACHINE ROTOR

• US 20140300240A1
• Filed: 04/04/2013
• Published: 10/09/2014
• Est. Priority Date: 04/04/2013
• Status: Abandoned Application

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Hochstetler, Derek R., Welch, Timothy R., Abels, Jan Henry
• Application Number:
  US13/856,718
• Publication Number:
  US 20140300240A1
• Time in Patent Office: Days
• US Class Current: 310/214
• CPC Class Codes: H02K 2213/03 Machines characterised by numerical values, ranges, mathematical expressions or similar information
• CPC Class Codes: H02K 3/487 Slot-closing devices
• CPC Class Codes: H02K 3/527 applicable to rotors only

Abstract

A wedge for a rotor of an electric machine includes a circumferentially outer surface defining a radial extent of the wedge extending from a first axial end of the wedge to a second axial end of the wedge. A plurality of circumferentially-extending grooves extend radially inwardly from the circumferentially outer surface to a groove depth. The plurality of grooves are axially spaced along a wedge length between the first axial end and the second axial end. The axial spacing between the grooves is greater than an axial width of each groove. An intermediate surface between adjacent grooves has a same radial position as a first end surface between the first axial end and a first groove closest to the first axial end. Two planar side surfaces circumferentially bound the circumferentially outer surface and extend radially inwardly from the cicumferential outer surface.

Claims

1. A wedge for a rotor of an electric machine comprising:

a circumferentially outer surface defining a radial extent of the wedge extending from a first axial end of the wedge to a second axial end of the wedge;

a plurality of circumferentially-extending grooves extending radially inwardly from the circumferentially outer surface to a groove depth, the plurality of grooves axially-spaced along a wedge length between the first axial end and the second axial end, the axial spacing between the grooves is greater than an axial width of each groove, an intermediate surface between adjacent grooves having a same radial position as a first end surface between the first axial end and a first groove closest to the first axial end; and

two planar side surfaces circumferentially bounding the circumferentially outer surface extending radially inwardly from the cicumferential outer surface.

2. The wedge of claim 1, wherein a ratio of wedge axial width to wedge axial spacing is between 0.6 and 0.7.

3. The wedge of claim 1, further comprising a circumferential inner surface extending between the two side surfaces and defining a radially inward extent of the wedge.

4. The wedge of claim 3, wherein the circumferential inner surface is planar.

5. The wedge of claim 3, wherein a ratio of an outer radius of curvature of the circumferentially outer surface to a normal distance from a center of curvature of the wedge to the circumferential inner surface is between 0.7 and 0.8.

6. The wedge of claim 1, further comprising a second end surface extending form a second axial end to a last groove closest to the second axial end, having a same radial position as the intermediate position.

7. The wedge of claim 6, wherein a ratio of a first end surface axial length to a second end surface axial length is not greater than 0.87.

8. The wedge of claim 1, wherein a ratio of the groove depth to a radius of curvature of the circumferentially outer surface is between 0.02 and 0.04.

9. A rotor assembly for a generator comprising:

a plurality of field coils;

a rotor core centered about a rotor axis and supportive of the plurality of field coils;

a plurality of rotor wedges, each rotor wedge assembled to the rotor core and abutting a field coil of the plurality of field coils to support and retain the field coil at the rotor core, each rotor wedge including;

a circumferentially outer surface defining a radial extent of the wedge extending from a first axial end of the wedge to a second axial end of the wedge;

a plurality of circumferentially-extending grooves extending radially inwardly from the circumferentially outer surface to a groove depth, the plurality of grooves axially-spaced along a wedge length between the first axial end and the second axial end, the axial spacing between the grooves is greater than an axial width of each groove, an intermediate surface between adjacent grooves having a same radial position as a first end surface between the first axial end and a first groove closest to the first axial end; and

two planar side surfaces circumferentially bounding the circumferentially outer surface extending radially inwardly from the cicumferential outer surface.

10. The rotor assembly of claim 9, wherein a ratio of wedge axial width to wedge axial spacing is between 0.6 and 0.7.

11. The rotor assembly of claim 9, wherein the wedge further includes a circumferential inner surface extending between the two side surfaces and defining a radially inward extent of the wedge.

12. The rotor assembly of claim 11, wherein the circumferential inner surface is planar.

13. The rotor assembly of claim 11, wherein a ratio of an outer radius of curvature of the circumferentially outer surface to a normal distance from the rotor axis to the circumferential inner surface is between 0.7 and 0.8.

14. The rotor assembly of claim 9, wherein the wedge further includes a second end surface extending form a second axial end to a last groove closest to the second axial end, having a same radial position as the intermediate position.

15. The rotor assembly of claim 14, wherein a ratio of a first end surface axial length to a second end surface axial length is not greater than 0.87.

16. The rotor assembly of claim 9, wherein a ratio of the groove depth to a radius of curvature of the circumferentially outer surface is between 0.02 and 0.04.

17. The rotor assembly of claim 9, wherein the rotor core comprises a plurality of rotor laminations stacked along the rotor axis.

18. The rotor assembly of claim 9, further comprising a rotor sleeve surrounding the rotor core and the plurality of rotor wedges to retain the rotor wedges at the rotor core.