Rotor assembly for an electric machine having a coolant passage

• US 10,554,088 B2
• Filed: 11/04/2013
• Issued: 02/04/2020
• Est. Priority Date: 09/06/2013
• Status: Active Grant

• Current Assignee: GE Aviation Systems LLC (General Electric Co. (Italy))
• Original Assignee: GE Aviation Systems LLC (General Electric Co. (Italy))
• Inventors: Huang, Hao, Jia, Xiaochuan, Zywot, Jan
• Primary Examiner(s): Lian, Mang Tin Bik
• Assistant Examiner(s): Almawri, Maged M
• Application Number:
  US15/029,917
• Publication Number:
  US 20160285332A1
• Time in Patent Office: 2,283 Days
• Field of Search: 310216, 310 61, 310433, 310216132, 310216086, 310216079, 310216074, 310216001, 310216013, 310216004, 310269, 310 52- 59, 3102611-266, 310216091
• CPC Class Codes: H02K 1/02 characterised by the magnetic material
• CPC Class Codes: H02K 1/24 Rotor cores with salient poles ; Variable reluctance rotors
• CPC Class Codes: H02K 1/26 Rotor cores with slots for windings
• CPC Class Codes: H02K 1/265 Shape, form or location of the slots
• CPC Class Codes: H02K 1/28 Means for mounting or fastening rotating magnetic parts on to, or to, the rotor structures
• CPC Class Codes: H02K 1/32 with channels or ducts for flow of cooling medium
• CPC Class Codes: H02K 1/325 between salient poles
• CPC Class Codes: H02K 19/02 Synchronous motors
• CPC Class Codes: H02K 19/16 Synchronous generators
• CPC Class Codes: H02K 19/38 Structural association of synchronous generators with exciting machines
• CPC Class Codes: H02K 3/18 Windings for salient poles
• CPC Class Codes: H02K 3/52 Fastening salient pole windings or connections thereto
• CPC Class Codes: H02K 3/527 applicable to rotors only
• CPC Class Codes: H02K 9/02 by ambient air flowing through the machine
• CPC Class Codes: H02K 9/197 in which the rotor or stator space is fluid-tight, e.g. to provide for different cooling media for rotor and stator
• CPC Class Codes: H02K 9/223 Heat bridges
• CPC Class Codes: H02K 9/227 Heat sinks

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 non-lamination structure defining a core rotational about an axis of rotation and having multiple posts and at least one projection disposed between the multiple posts;

a winding wound around each of the multiple posts;

a winding seat located at an interface of the winding and each of the multiple posts, the winding seat spaced from the at least one projection, having at least two surfaces and defining an electrically isolating layer separating the winding from each of the multiple posts;

a lamination structure defining a cap coupled to each of the multiple posts, and having a portion overlying the winding to collectively define an axial extending winding slot with the core;

at least one internal coolant passage located internally of the core adjacent to and at least partially separated from the winding by the winding seat, wherein one of the at least two surfaces of the winding seat is adjacent to the portion of each of the multiple posts, and extends axially in parallel with the internal coolant passage;

a central coolant passage extending axially along the axis of rotation within the core; and

at least one radial coolant passage extending outward from the central coolant passage to fluidly couple the at least one coolant passage to the central coolant passage;

wherein adjacent caps coupled to each of the multiple posts are spaced from each other by a radial element coupled to the at least one projection.

2. The rotor assembly of claim 1 wherein the central coolant passage comprises a bore in the core.

3. The rotor assembly of claim 1 wherein the internal coolant passage, central coolant passage, and the at least one radial coolant passage together form part of a coolant loop.

4. The rotor assembly of claim 3 wherein at least a portion of the at least one radial coolant passage extends along a channel adjacent another of the at least two surfaces of the winding seat.

5. The rotor assembly of claim 1 wherein the core further comprises a thermal conductor provided on the winding seat.

6. The rotor assembly of claim 5 wherein the thermal conductor is a coating applied to the winding seat.

7. The rotor assembly of claim 1 further comprising at least one wedge configured to bias the winding into the winding seat.

8. The rotor assembly of claim 7 wherein the at least one wedge comprises a biasing element.

9. The rotor assembly of claim 1 wherein the cap is made from material that is less electrically conductive than the core.

10. The rotor assembly of claim 9 wherein the core is made from material that is thermally more conductive than the cap.

11. The rotor assembly of claim 9 wherein in the cap is made from cobalt and the core is made from steel.

12. A rotor assembly for an electric machine comprising:

a non-lamination structure defining a core rotational about an axis of rotation and having multiple posts and at least one projection disposed between the multiple posts and a central coolant passage extending axially along the axis of rotation;

a winding wound around each of the multiple posts;

a winding seat located at an interface of the winding and each of the multiple posts, the winding seat spaced from the at least one projection, having at least two surfaces and defining an electrically isolating layer separating the winding from each of the multiple posts;

a lamination structure defining a cap coupled to each of the multiple posts and having a portion overlying the winding to collectively define an axial extending winding slot with the core;

a channel adjacent the winding seat; and

at least one radial coolant passage extending outward from the central coolant passage to fluidly couple the central coolant passage to the channel;

wherein adjacent caps coupled to each of the multiple posts are spaced from each other by a radial element coupled to the at least one projection.

13. The rotor assembly of claim 12 further comprising at least one internal coolant passage located internally of the core, radially spaced from the central coolant passage, fluidly coupled with the central coolant passage by the at least one radial coolant passage, and adjacent to and separated from the winding seat.

14. The rotor assembly of claim 13 wherein the at least one internal coolant passage, the at least one radial coolant passage, and the central coolant passage at least partially form a coolant loop entirely internal to the core.

15. The rotor assembly of claim 14 wherein the core further comprises a first radial passage proximate to a first axial end of the core and a second radial passage proximate to a second opposite axial end of the core, and wherein the first and second radial passages form part of the coolant loop.

16. The rotor assembly of claim 15 wherein the first radially passage is a portion of the coolant loop to deliver coolant flow from the central passage to the internal coolant passage and wherein the second radially passage is a portion of the coolant loop to return coolant flow from the internal coolant passage to the central passage.