Magnetic bearing assembly having inner ventilation

Abstract

A magnetic bearing assembly for a rotary machine having a rotor shaft, comprising a stator magnetic circuit secured to a stationary support element and comprising at least one body of ferromagnetic material and at least one coil, both being fitted in a protective annular housing leaving uncovered a surface of revolution of said ferromagnetic body and a surface of revolution of said one coil, the magnetic bearing assembly comprising an annular thrust collar secured to the rotor shaft and radially extending towards the stator magnetic circuit by a radial portion, said radial portion facing the uncovered surfaces of said ferromagnetic body and said one coil. The annular thrust collar comprises at least one flow channel.

Claims

1. A magnetic bearing assembly for a rotary machine having a rotor shaft, the bearing assembly comprising: a stator magnetic circuit secured to a stationary support element and comprising at least one body of ferromagnetic material and at least one coil, both the at least one body of ferromagnetic material and the at least one coil being fitted in a separate protective annular housing having a slot therein configured to receive the at least one body of ferromagnetic material, and leaving uncovered only a surface of revolution of said ferromagnetic body and a surface of revolution of said one coil, wherein the annular housing is arranged between the ferromagnetic body and the stationary support element in a radial direction, and an annular thrust collar secured to the rotor shaft and radially extending towards the stator magnetic circuit by a radial portion, said radial portion facing the uncovered surfaces of said ferromagnetic body and said one coil, wherein the annular thrust collar comprises at least one flow channel extending from an outer cylindrical surface of the radial portion towards the rotor shaft, wherein the annular housing is arranged between the ferromagnetic body and the annular thrust collar in the radial direction, wherein said at least one flow channel is a plurality of angled radial grooves each provided on at least one lateral surface of the radial portion of the annular thrust collar and opening on an outer cylindrical surface of the rotor shaft.

2. The bearing assembly according to claim 1, wherein each of the plurality of radial grooves is radially and tangentially shaped.

3. The bearing assembly according to claim 1, wherein the stator magnetic circuit comprises two bodies of ferromagnetic material, each facing one lateral surface of the radial portion of said annular thrust collar.

4. The bearing assembly according to claim 1, wherein the magnetic bearing assembly is an axial magnetic bearing.

5. A turbomachine comprising: a stator, a rotor mounted in rotation in said stator, and at least one magnetic bearing assembly according to claim 1.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Embodiments of the present invention will be better understood from studying the detailed description of a number of embodiments considered by way of entirely non-limiting examples and illustrated by the attached drawings in which:

(2) FIG. 1 is an axial half-section of the axial magnetic bearing assembly according to an embodiment of the invention mounted between two components of a motor;

(3) FIG. 2 is an axial half-section of a thrust collar along line II-II of FIG. 1 according to an embodiment of the invention;

(4) FIG. 3 is an half view of the thrust collar of FIG. 1 mounted on a rotor according to an embodiment of the invention;

(5) FIG. 4 is an axial half-section of a thrust collar according to an embodiment of the invention;

(6) FIG. 5 is an half view of the thrust collar of FIG. 4 mounted on a rotor according to an embodiment of the invention.

DETAILED DESCRIPTION

(7) The following detailed description of the exemplary embodiments refers to the accompanying drawings. The same reference numbers in different drawings identify the same or similar elements. Additionally, the drawings are not necessarily drawn to scale.

(8) As illustrated on FIG. 1, a magnetic bearing, designed by general reference number 10, is designed to be mounted in a rotary machine (not shown) comprising a casing or housing, a rotating shaft 12 extending along an axis X-X and adapted to support a rotor part (not shown). For example, if the rotating machine is a centrifugal compressor, the rotor part comprises impellers. The rotating shaft 12 and the associated rotor part form a rotor assembly.

(9) As illustrated on FIG. 1, the magnetic bearing 10 is of the axial type and is designed to support the rotor shaft 12 inside the stator casing. A radial type magnetic bearing (not shown) may also be associated to the axial magnetic bearing 10 to support the rotating shaft 12.

(10) The active magnetic bearing 10 comprises a stator armature 14 fixed to the stator casing and a rotor armature 16 or annular thrust collar having the shape of a disk secured to the rotating shaft 12. The annular thrust collar 16 extends radially from an axial plate 16a secured to the rotor shaft 12 towards the stator magnetic circuit 18 by a radial portion 16b having an outer cylindrical surface 16c and two lateral surfaces 16d, 16e.

(11) The stator armature 14 comprises a stator magnetic circuit 18 including, in conventional manner, one or more annular coils 20 and two ferromagnetic bodes 22 which may be massive or laminated locally. In the example of FIG. 1, each ferromagnetic body 22 encloses two annular coils 20. The stator armature 14 also comprises a protective annular support or annular housing 24 into which is placed the stator magnetic circuit 18, leaving uncovered a surface of revolution 22a of the ferromagnetic bodes 22 and a surface 20a of revolution of each coils 20. The support 24 is secured to a stationary support element 26 that is itself fixed to the casing.

(12) As illustrated, the radial portion 16b of the thrust collar 16 faces the uncovered surfaces 20a, 22a respectively of each ferromagnetic bodies 22 and each coils 20. In other words, the stator magnetic circuit 18 is placed axially facing the annular thrust collar 16 with no mechanical contact, leaving an axial gap 28 between the annular thrust collar 16 and the stator magnetic circuit 18.

(13) The rotation shaft 12 may be provided with a stepped profile 12a for an axial positioning of the thrust collar 16. The annular thrust collar 16 could, for example, be made integrally with the rotor shaft 12.

(14) As illustrated on FIGS. 2 and 3, the annular thrust collar 16 comprises a plurality of grooves 30 on each radial lateral surface 16d, 16e of the radial portion 16b. The grooves 30 act as flow channels for the flow of the fluid. The flow channels 30 extend from the outer cylindrical surface 16c of the radial portion 16b towards the rotor shaft 12 and are inclined grooves directed radially towards the shaft 12 and are provided on the lateral surface 16d of the radial portion 16b of the thrust collar 16. As illustrated, the grooves 30 are shaped radially and tangentially to the outer cylindrical surface 16c of the radial portion 16b.

(15) As illustrated on FIG. 3, the flow channels 30 are be provided on both lateral surfaces 16d, 16e of the radial portion 16b of the thrust collar 16. Alternatively, flow channels can be provided only on one lateral surface of the thrust collar 16.

(16) As illustrated, the flow channels 30 opens on the axial plate 16a of the thrust collar 16. Alternatively, the flow channels can open on the outer cylindrical surface 12b of the rotor shaft 12. The fluid inside the turbomachine flows through the air gap 28 and inside the flow channels 30. The direction of flow is shown by the arrow F.

(17) Such flow channels 30 increase the ventilation inside the magnetic bearing and allow the magnetic bearing to be cooled.

(18) The embodiment shown in FIGS. 4 and 5, in which identical parts bear the same reference, is substantially different from the embodiment of FIGS. 2 and 3 in the location of the flow channels.

(19) As illustrated on FIGS. 4 and 5, the thrust collar 16 is provided with a plurality of grooves 32 provided inside the radial portion 16b. The grooves 32 act as flow channels for the fluid and open only at the outer cylindrical surface 16c of the radial portion 16b. Alternatively, the flow channels can open on the outer cylindrical surface 12b of the rotor shaft 12.

(20) The groove 32 are inclined and radially directed towards the shaft 12. As illustrated, the grooves 32 are shaped radially and tangentially to the outer cylindrical surface 16c of the radial portion 16b.

(21) A benefit of an embodiment of the present invention, is the axial magnetic bearing assembly has enhanced cooling flow. T flow channels facilitate the pumping of the flow of fluid enhancing the cooling of the active magnetic bearing. The magnetic bearing is thus provided with inner ventilation.

(22) This written description uses examples to disclose the invention, including the preferred embodiments, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.