Rotor assembly for an electric machine

• US 9,837,868 B2
• Filed: 02/28/2014
• Issued: 12/05/2017
• Est. Priority Date: 02/28/2014
• Status: Active Grant

• Current Assignee: GE Aviation Systems LLC (GE Aerospace)
• Original Assignee: GE Aviation Systems LLC (GE Aerospace)
• Inventors: Wirsch, Jr., Paul James, Huang, Hao, Jia, Xiaochuan, Zywot, Jan
• Primary Examiner(s): Mok, Alex W
• Application Number:
  US14/193,666
• Publication Number:
  US 20150249370A1
• Time in Patent Office: 1,376 Days
• Field of Search: 310 54
• CPC Class Codes: H02K 3/18 Windings for salient poles
• CPC Class Codes: H02K 3/24 with channels or ducts for cooling medium between the conductors
• CPC Class Codes: H02K 3/527 applicable to rotors only

Abstract

A rotor assembly for an electric machine includes a core having at least one post and a cap wherein electrical windings are wound about the rotor assembly to define a pole. The rotation of the rotor and rotor pole relative to a stator generates a current supplied from the electric machine to a power consuming device.

Claims

1. A rotor assembly for an electric machine comprising:

a rotor core having at least one post and a set of coolant passages included in a rotor of the rotor core;

a winding wound around the post having axial segments that run along a opposite first and second sides of the post, and an end portion extending axially beyond a third side of the post, connecting the axial segments, to define an end turn segment, wherein the post at least partially defines a first face for receiving the winding; and

a coolant tube, that at least partially encompasses the post and defines a second face for receiving the rotor windings, wherein the coolant tube is located adjacent to, and extending axially in parallel with, the axial segments and at least partially extending in parallel with the end turn segment; and

an end tube transition that defines a transition portion of the coolant tube, and fluidly couples the coolant tube to the set of coolant passages included in the rotor,

wherein the coolant tube has at least a portion in a thermally conductive relationship with at least a portion of the end turn segment, wherein heat from the end turn segment is transferred by conduction to the at least a portion of the coolant tube.

2. The rotor assembly of claim 1 wherein at least 90% of the end turn segment is in a thermally conductive relationship with the at least a portion of the coolant tube.

3. The rotor assembly of claim 2 wherein at least 90% of the end turn segment is in a thermally conductive relationship with at least a portion of the multiple coolant tubes, collectively.

4. The rotor assembly of claim 1 further comprising multiple coolant tubes wherein the multiple coolant tubes are in a thermally conductive relationship with at least a portion of each end turn segment.

5. The rotor assembly of claim 1 wherein the end tube transitions extend away from the end turn segment to define the transition portion.

6. The rotor assembly of claim 5 wherein the end tube transition portion has an arcuate shape.

7. The rotor assembly of claim 1 further comprising a thermally conductive layer provided on the winding.

8. The rotor assembly of claim 7 wherein the thermally conductive layer is a coating applied to the winding.

9. The rotor assembly of claim 7 wherein the thermally conductive layer is a fin assembly configured about the winding.

10. The rotor assembly of claim 9 wherein the fin assembly comprises at least two fins in a thermally conductive relationship with multiple faces of the at least one coolant tube.

11. The rotor assembly of claim 1 wherein the thermally conductive relationship does not comprise an air gap.

12. The rotor assembly of claim 1, wherein the coolant tube has substantially trapezoidal geometric cross section.

13. The rotor assembly of claim 1, further comprising at least one of a slot liner or fin assembly configured to provide a thermally conductive relationship between the winding and the coolant tube.

14. A rotor assembly for an electric machine comprising:

a rotor core having at least one post at least partially defining a first face of a winding seat, and coolant passages included in a rotor of the rotor core;

a set of coolant tubes encompassing a portion of the at least one post, and at least partially defining a second face of the winding seat;

a winding wound around the post and at least partially supported by the winding seat, wherein the winding extending axially beyond the post define an end turn segment,

wherein a portion of the set of coolant tubes is adjacent to, and at least partially in parallel with end turn segment, and in a thermally conductive relationship with at least a portion of the end turn segment; and

a set of end tube transitions that define transition portions of coolant tubes in the set of coolant tubes, and fluidly couple the set of coolant tubes to the coolant passages included in the rotor.

15. The rotor assembly of claim 14, wherein the end tube transitions extend away from the end turn segment.

16. The rotor assembly of claim 15, wherein the end tube transition portion has an arcuate shape.