Magnetic thrust bearings

• US 8,963,393 B2
• Filed: 12/18/2012
• Issued: 02/24/2015
• Est. Priority Date: 12/18/2012
• Status: Expired due to Fees

• Current Assignee: ABB Schweiz AG (ABB Limited)
• Original Assignee: ABB Research Ltd. (ABB Limited)
• Inventors: Upadhyay, Parag
• Primary Examiner(s): NGUYEN, HANH N
• Application Number:
  US13/718,482
• Publication Number:
  US 20140167543A1
• Time in Patent Office: 798 Days
• Field of Search: 310/90.5, 310/178, 310/181
• US Class Current: 310/90.5
• CPC Class Codes: F16C 32/0468 of moving parts of the magnetic circuit, e.g. of the rotor
• CPC Class Codes: F16C 32/0476 with active support of one degree of freedom, e.g. axial magnetic bearings
• CPC Class Codes: H02K 7/09 with magnetic bearings

Abstract

Rotating machines and magnetic thrust bearings therefor are disclosed. Magnetic thrust bearings may include a rotor core configured to extend coaxially around a shaft of a rotating machine, a non-magnetic element configured to be coaxially disposed on the shaft, and a stator comprising a stator core and a coil, both of which are configured to extend coaxially around the axis. The rotor core may include a substantially radially extending thrust face and a substantially axially extending peripheral surface. The non-magnetic element may radially space the thrust face from the shaft. The stator core may include a substantially radially extending first pole surface and a substantially axially extending second pole surface. The first pole surface may define an axial air gap with the thrust face, and the second pole surface may define a radial air gap with the peripheral surface.

Claims

1. A magnetic thrust bearing for a rotating machine having a shaft extending along an axis, the magnetic thrust bearing comprising:

a rotor core configured to extend coaxially around the shaft, the rotor core having a substantially radially extending thrust face and a substantially axially extending peripheral surface;

a non-magnetic element configured to be coaxially disposed on the shaft, wherein the non-magnetic element radially spaces the thrust face from the shaft; and

a stator comprising a stator core and a coil both configured to extend coaxially around the axis, wherein the stator core comprises a substantially radially extending first pole surface and a substantially axially extending second pole surface, the first pole surface defines an axial air gap with the thrust face, and the second pole surface defines a radial air gap with the peripheral surface.

2. The magnetic thrust bearing of claim 1, wherein the thrust face is perpendicular to the axis.

3. The magnetic thrust bearing of claim 1, wherein the peripheral surface extends parallel to the axis.

4. The magnetic thrust bearing of claim 1, wherein the axial and radial air gaps are radially spaced apart.

5. The magnetic thrust bearing of claim 1, wherein the axial and radial air gaps are axially spaced apart.

6. The magnetic thrust bearing of claim 1, wherein the axial air gap radially extends from an outer surface of the non-magnetic element to a peripheral edge of the thrust face.

7. The magnetic thrust bearing of claim 6, wherein the peripheral edge of the thrust face is radially aligned with the peripheral surface of the rotor core.

8. The magnetic thrust bearing of claim 6, wherein the peripheral surface of the rotor core is disposed radially outward from the peripheral edge of the thrust face.

9. The magnetic thrust bearing of claim 1, wherein the non-magnetic element is configured to radially space the rotor core from an exterior surface of the shaft.

10. The magnetic thrust bearing of claim 9, wherein the non-magnetic element comprises an axially extending outer surface and the stator core comprises an axially extending inner surface that is substantially radially aligned with the outer surface of the non-magnetic element.

11. The magnetic thrust bearing of claim 1, wherein at least one of the rotor core and the stator comprises an annular structure configured to extend substantially completely circumferentially around the axis.

12. The magnetic thrust bearing of claim 1 incorporated into a rotating machine, the rotating machine comprising:

the shaft; and

at least one magnetic thrust bearing of claim 1 configured to axially support the shaft, wherein the rotor core extends coaxially around the shaft, the non-magnetic element is coaxially disposed on the shaft, and the stator core and the coil both extend coaxially around the shaft.

13. The rotating machine of claim 12, comprising at least two magnetic thrust bearings of claim 1 configured to axially support the shaft, wherein the thrust faces of the rotor cores of the at least two magnetic thrust bearings are oriented in the same direction.

14. The rotating machine of claim 12, comprising two magnetic thrust bearings of claim 1 configured to axially support the shaft, wherein the thrust faces of the rotor cores of the two magnetic thrust bearings are oriented in opposite directions.

15. A rotating machine, comprising:

a shaft having an exterior surface;

a magnetic thrust bearing rotor core extending coaxially around the shaft, the magnetic thrust bearing rotor core having a radially extending thrust face and an axially extending peripheral surface;

a magnetic thrust bearing stator comprising a coil and a stator core that both extend coaxially around the shaft, wherein the stator core comprises a radially extending pole surface and an axially extending pole surface, the radially extending pole surface defining an axial air gap with the thrust face, and the axially extending pole surface defining a radial air gap with the peripheral surface; and

a non-magnetic element disposed around the exterior surface of the shaft, wherein the non-magnetic element radially spaces the axial air gap from the exterior surface of the shaft.

16. The rotating machine of claim 15, wherein the non-magnetic element radially spaces the magnetic thrust bearing rotor core from the exterior surface of the shaft.

17. The rotating machine of claim 16, wherein the non-magnetic element comprises an axially extending outer surface and the stator core comprises an axially extending inner surface that is substantially radially aligned with the outer surface of the non-magnetic element.

18. The rotating machine of claim 15, wherein the axial and radial air gaps are spaced apart at least one of axially and radially.

19. The rotating machine of claim 15, wherein the axial air gap radially extends from an outer surface of the non-magnetic element to a peripheral edge of the thrust face.

20. The rotating machine of claim 19 wherein the peripheral edge of the thrust face is radially aligned with the peripheral surface of the rotor core.