ELECTRIC MACHINE HAVING ROTOR COOLING ASSEMBLY

• US 20150280522A1
• Filed: 03/31/2014
• Published: 10/01/2015
• Est. Priority Date: 03/31/2014
• Status: Abandoned Application

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: AUSTIN, Gregory Thomas, BAUMANN, Jonathan Mathew, NAHRWOLD, Thomas Lee, TIGUE, Joseph Daniel, SCHLACK, Timothy James, BUATTE, Vance Michael
• Application Number:
  US14/230,830
• Publication Number:
  US 20150280522A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: H02K 9/19 for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil

Abstract

A cooling assembly is disclosed for use with an electric machine having bearings, a shaft rotatably supported by the bearings, a rotor connected to the shaft, and a stator annularly surrounding the rotor. The cooling assembly may have an end cap configured to engage an end of the rotor and the shaft to thereby axially locate the rotor relative to the shaft. The end cap may include an annular groove formed therein to receive a flow of cooling oil. The cooling assembly may further have an annular baffle axially connected to an end of the end cap and extending radially inward at least partially across an opening of the annular groove, and a slinger axially connected to the annular baffle opposite the end cap. The slinger may include a recess formed therein that is configured to trap the cooling oil after it flows through the annular baffle.

Claims

1. An end cap for a rotor, comprising:

a ring-shaped body having an inner axial surface that is generally planar and configured to engage the rotor, and an outer axial surface that is located opposite the inner axial surface; and

an annular groove formed within the outer axial surface, the annular groove having an inner radial side surface with concave curvature.

3. The end cap of claim 1, wherein the annular groove further includes an outer radial side surface that is generally planar and tilted axially outward.

2. The end cap of claim I, wherein a cross-section of the annular groove is asymmetrical.

4. The end cap of claim I, wherein the annular groove has a flat axial bottom, and the inner radial side surface is tangential with the flat axial bottom.

5. The end cap of claim I, further including an inner annular flange configured to engage a shaft and thereby axially locate the rotor relative to the shaft.

6. A cooling assembly for an electric machine having bearings, a shaft rotatably supported by the bearings, a rotor connected to the shaft, and a stator annularly surrounding the rotor, the cooling assembly comprising:

an end cap configured to engage an end of the rotor and the shaft to thereby axially locate the rotor relative to the shaft, the end cap having an annular groove formed therein to receive a flow of cooling oil;

an annular baffle axially connected to an end of the end cap and extending radially inward at least partially across an opening of the annular groove; and

a slinger axially connected to the annular baffle opposite the end cap, the slinger forming a channel that is configured to trap cooling oil after it flows past the annular baffle.

7. The cooling assembly of claim 6, wherein the annular baffle includes at least one axial hole configured to allow passage of the cooling oil from the annular groove of the end cap into the channel of the slinger.

8. The cooling assembly of claim 7, wherein the at least one axial hole includes at least two axial holes located at diametrically opposing sides of the annular baffle.

9. The cooling assembly of claim 8, wherein the at least two holes includes two pairs of two holes, each pair of two holes being located at diametrically opposing sides of the annular baffle.

10. The cooling assembly of claim 6, wherein the annular baffle extends radially inward a greater distance than the slinger.

11. The cooling assembly of claim 6, wherein the channel has an axial depth that is less than an axial depth of the annular groove in the end cap.

12. The cooling assembly of claim 6, wherein:

the end cap, the annular baffle, and the slinger each includes a plurality of holes located around a. periphery; and

the cooling assembly further includes a plurality of fasteners configured to pass through the plurality of holes and clamp the slinger, the annular baffle, and the end cap to each other.

13. The cooling assembly of claim 6, further including:

a housing configured to secure the bearings; and

a cooling passage formed within walls of the housing and configured to direct the flow of cooling oil axially into the annular groove, past the slinger and the annular baffle.

14. The cooling assembly of claim 13, wherein the cooling passage includes an axial portion formed radially outward of the bearings.

15. The cooling assembly of claim 14, wherein the cooling passage further includes a radial portion passing through an axial end wall of the housing to supply cooling oil to the axial portion at the bearings.

16. The cooling assembly of claim 13, wherein:

the end cap is a first end cap configured to engage a first end of the rotor and the shaft;

the annular baffle is a first annular baffle connected to an end of the first end cap;

the slinger is a first slinger axially connected to the first annular baffle;

cooling passage is a first cooling passage; and

the cooling assembly further includes;

a second end cap configured to engage a second end of the rotor and the shaft, and having a second annular groove;

a second annular baffle connected to an end of the second end cap;

a second slinger axially connected to the second annular baffle; and

a second cooling passage formed within the walls of the housing and configured to direct the flow of cooling oil axially into the second annular groove, past the second slinger and the second annular baffle.

17. A method of cooling an electric machine, comprising:

directing cooling oil axially into an annular groove in a rotor end cap;

directing the cooling oil to circulate radially outward within the annular groove;

directing the cooling oil axially out of the annular groove and into a radial channel; and

allowing the cooling oil to move radially inward and spill over a lip at an axial end of the radial channel.

18. The method of claim 17, wherein directing the cooling oil axially into the annular groove includes directing the cooling oil against a concave radially inner surface of the annular groove at a single location.

19. The method of claim 19, wherein directing the cooling oil axially out of the annular groove includes directing the cooling oil through a hole in an annular baffle.

20. The method of claim 19, wherein directing the cooling oil axially out of the annular groove includes directing the cooling oil into the radial channel from multiple locations around the annular groove.