Landing bearing assembly and rotary machine equipped with such an assembly and a magnetic bearing

Patent metadata

Field	Value
Publication number	US-10859115-B2
Application number	US-201715682950-A
Country	US
Kind code	B2
Filing date	Aug 22, 2017
Priority date	Aug 31, 2016
Publication date	Dec 8, 2020
Grant date	Dec 8, 2020

Abstract

A landing bearing assembly for a rotary machine having a stator assembly, a rotor assembly and a magnetic bearing. The landing bearing assembly having a stator landing portion integral with the stator assembly and a rotor landing portion integral with the rotor assembly. A first coating, which is an anti-wear and/or an anti-friction coating, is dispensed on at least one of the stator landing portion and the rotor landing portion. The invention also concerns such a rotary machine.

First claim

The invention claimed is:

1. A landing bearing assembly for a rotary machine comprising:
a stator landing portion configured to be engageable with a stator assembly of the rotary machine;
a rotor landing portion integral with a rotor assembly of the rotary machine,
wherein the stator landing portion and the rotor landing portion comprise a corrosion resistance material;
wherein the stator assembly comprises a first stator axial end and a second stator axial end, a lateral holder being disposed adjacent to the first stator axial end and a backing device being disposed adjacent to the second stator axial end, wherein the lateral holder and the backing device are configured to fasten the stator landing portion to the stator assembly;
wherein the rotor landing portion comprises a landing sleeve, the landing sleeve comprising an axial portion and a first radial portion, the first radial portion radially extending from a first axial end of the axial portion; and
a first coating dispensed on the first radial portion and axial portion of the landing sleeve, the first coating being an anti-wear or an anti-friction coating.

2. The landing bearing assembly according to claim 1 , wherein the first coating is also located on an inner ring of a bearing of the stator landing portion.

3. The landing bearing assembly according to claim 2 , wherein the first coating is made of alumines in a matrix of titanium, and
wherein a sub-layer of nickel-aluminium alloy is first applied.

4. The landing bearing assembly according to claim 1 , wherein the first coating is made of tungsten carbide in a matrix of cobalt-chrome.

5. The landing bearing assembly according to claim 1 , further comprising a second coating made of diamond like carbon is applied onto the first coating.

6. The landing bearing assembly according to claim 1 , wherein the corrosion resistance material of the stator landing portion comprises a high nitrogen steel.

7. The landing bearing assembly according to claim 1 , wherein the corrosion resistance material of the rotor landing portion comprises a nickel based alloy.

8. The landing bearing assembly according to any claim 1 , wherein the stator landing portion consists of a double row angular contact ball bearing or a pair of single row angular contact bearings.

9. The landing bearing assembly according to claim 1 , wherein the stator landing portion consists of a single ring.

10. The landing bearing assembly according to claim 1 , wherein the landing sleeve has a U-shape.

11. The landing bearing assembly according to claim 1 , wherein the rotor landing portion forms part of the rotor shaft itself.

12. The landing bearing assembly according to claim 1 , wherein a thickness of the first coating is between one tenth and ten tenths of a millimeter.

13. A The rotary machine comprising:
the landing bearing assembly of claim 1 , and
a magnetic bearing.

14. The rotary machine according to claim 13 , wherein the landing sleeve comprises a second radial portion which extends radially from a second axial end of the axial portion, the first coating being located on the second radial portion such that the first coating forms a U-shape on the landing sleeve.

15. The landing bearing assembly according to claim 1 , wherein a thickness of the first coating is between one tenth and ten tenths of a millimeter.

16. The landing bearing assembly according to claim 1 , wherein the first coating is corrosion resistant and operates in direct contact with a corrosive fluid for cooling.

17. The landing bearing assembly according to claim 1 , wherein the landing sleeve comprises a second radial portion which extends radially from a second axial end of the axial portion, the first coating being located on the second radial portion such that the first coating forms a U-shape on the landing sleeve.

18. The landing bearing assembly according to claim 17 , wherein the stator landing portion comprises a bearing having an inner ring, the landing sleeve and the first coating defining a recess configured to receive the bearing therein, when the bearing is seated with the inner ring abutting the first coating along the axial portion of the landing sleeve a portion of the inner ring extends radially out of the recess and radially past the first and second radial portions of the landing sleeve.

19. The landing bearing assembly according to claim 17 , further comprising a second coating, of different material from the first coating, being located on the first coating, wherein the stator landing portion comprises a bearing having an inner ring, the landing sleeve, the first coating, and the second coating defining a recess configured to receive the bearing therein, when the bearing is seated with the inner ring abutting the second coating along the axial portion of the landing sleeve a portion of the inner ring extends radially out of the recess and radially past the first and second radial portions of the landing sleeve.

20. A rotary machine comprising:
a stator assembly,
a stator landing portion configured to be engageable with the stator assembly, the stator landing portion having an axially extending radially inner surface,
the stator landing portion further comprising a tubular bush disposed on the axially extending radially inner surface thereof,
the stator landing assembly further comprising a bearing disposed on the tubular bush thereof,
a rotor landing portion integral with a rotor assembly of the rotary machine, wherein the stator landing portion and the rotor landing portion comprise a corrosion resistance material,
wherein the rotor landing portion comprises a landing sleeve, the landing sleeve comprising an axial portion and a first radial portion, the first radial portion radially extending from a first axial end of the axial portion;
a first coating dispensed on the first radial portion and axial portion of the landing sleeve, the first coating being an anti-wear or an anti-friction coating,
the axial portion defining a first piece of the landing sleeve and the first radial portion defining a second piece of the landing sleeve, the first piece and the second piece being separated by the first coating,
the stator assembly having first and second stator axial ends, a lateral holder disposed adjacent to the first stator axial end,

a backing device disposed adjacent to the second stator axial end, wherein the lateral holder and the backing device are configured to fasten the stator landing portion to the stator assembly; and prevent the bearing from moving axially relative to the stator landing portion.

Assignees

• Skf Magnetic Mechatronics

Inventors

• Anders Jens

Classifications

• F16C35/073 Primary

  between shaft and inner race ring · CPC title

• F16C2206/00

  Materials with ceramics, cermets, hard carbon or similar non-metallic hard materials as main constituents · CPC title

• F16C32/0442

  with devices affected by abnormal, undesired or non-standard conditions such as shock-load, power outage, start-up or touchdown · CPC title

• H02K7/09

  with magnetic bearings · CPC title

• F16C35/077

  between housing and outer race ring · CPC title