IP Library › Granted Patent US 11,025,114
Granted Patent B2
US 11,025,114 · App. 16/233,456 · Granted Jun 1, 2021

Rotor for an electric machine

Inventors: Balamurugan Sridharan (Karnataka, IN); Rajendra Vishwanath Pawar (Karnataka, IN); Mamatha Ramakrishnaiah (Karnataka, IN); Xiaochuan Jia (Centerville, OH); Samir Dey (Mason, OH); Hao Huang (Troy, OH); Dhiraj Khushal Thakare (Karnataka, IN); Pankaj Kumar Morya (Karnataka, IN)
Assignee: GE Aviation Systems LLC
H02K1/32H02K1/16H02K1/28H02K3/24H02K3/50H02K9/19
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Quick Facts
Patent No.
US 11,025,114
App. No.
16/233,456
Granted
Jun 1, 2021
Kind
B2
Abstract

A rotor for an electric machine includes a core having circumferentially-spaced, axially-extending posts, and defining an axial passage, a winding carried by each of the posts and comprising an electrically-conductive wire repeatedly wound around the post such that a portion of the winding extends axially beyond the post to define an overhang with upper and lower surfaces connected by an end, and a hollow shaft defining a rotor inner surface and a rotor outer surface.

Claims (28)

1. A rotor for an electric machine comprising:

a core having circumferentially-spaced, axially-extending posts;

a winding carried by each of the posts and comprising an electrically-conductive wire repeatedly wound around the post such that a portion of the winding extends axially beyond the post to define an overhang with upper and lower surfaces connected by an axially-facing end; and

a cradle supporting at least the lower surface of the overhang and having a first coolant opening fluidly coupled to the overhang lower surface, and a second coolant opening fluidly coupled to axially facing end of the overhang;

wherein the coolant is received through the first coolant opening and expelled through the second coolant opening.

2. The rotor of claim 1 wherein the cradle supports at least one of the upper surface and end.

3. The rotor of claim 1 wherein the cradle supports the upper surface and end.

4. The rotor of claim 1 wherein the cradle overlies the upper surface of the overhang and defines a second coolant opening with the core.

5. The rotor of claim 4 wherein the cradle is spaced from the core to form a gap that defines the second coolant opening.

6. The rotor of claim 5 wherein the gap is axially aligned with a set of stator winding end turns radially spaced from the winding.

7. The rotor of claim 6 wherein the gap is a coolant outlet configured to radially emit a coolant toward the set of stator winding end turns.

8. The rotor of claim 7 , further comprising an axial-facing wall proximate to the gap, wherein the wall is adapted to direct a coolant flow gathered at the wall toward the coolant outlet.

9. The rotor of claim 1 wherein the core defines an axial passage and further comprising a shaft located within the axial passage.

10. The rotor of claim 9 wherein the shaft comprises a coolant passage fluidly coupled to the first coolant opening.

11. The rotor of claim 10 wherein the shaft is hollow defining a rotor inner surface and a rotor outer surface, and the coolant passage extends between the inner and outer surfaces.

12. The rotor of claim 1 wherein the winding is a set of exciter windings.

13. A rotor for an electric machine comprising:

a core having circumferentially-spaced, axially-extending posts, and defining an axial passage;

a winding carried by each of the posts and comprising an electrically-conductive wire repeatedly wound around the post such that a portion of the winding extends axially beyond the post to define an overhang with upper and lower surfaces connected by an end;

a hollow shaft defining a rotor inner surface and a rotor outer surface; and

a cradle having a collar circumscribing the outer surface of the hollow shaft and a C-shaped channel supported by the collar and defining a first wall confronting the lower surface, a second wall confronting the upper surface, and a third wall confronting the end, with at least one of the first, second, and third walls having a coolant opening fluidly coupled to the overhang;

wherein coolant is received through the coolant opening in the first wall, expelled through the coolant opening in the second wall, and expelled axially through the coolant opening in the third wall.

14. The rotor of claim 13 wherein the first and third walls having coolant openings.

15. The rotor of claim 14 wherein the coolant openings are slots.

16. The rotor of claim 13 wherein the shaft has at least one coolant passage extending between the inner and outer surfaces.

17. The rotor of claim 13 wherein the second wall terminates short of the core to define a gap that is fluidly coupled to the coolant opening to define a coolant path through the overhang.

18. The rotor of claim 17 wherein the gap is axially aligned with a set of stator winding end turns radially spaced from the winding.

19. The rotor of claim 13 wherein the winding is a set of exciter windings.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 8, 2019
From: SRIDHARAN, BALAMURUGAN; PAWAR, RAJENDRA VISHWANATH; RAMAKRISHNAIAH, MAMATHA; JIA, XIAOCHUAN; DEY, SAMIR; HUANG, HAO; THAKARE, DHIRAJ KHUSHAL; MORYA, PANKAJ KUMAR
To: GE AVIATION SYSTEMS LLC
Reel/Frame 047933/0133 →
Continuity (1)
Related Publication 20200212742A1 · Jul 2, 2020
Cited By (7)
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