Thrust bearing, a turbomachine, and a method of making a bearing rotor disk for an electromagnetic thrust bearing in a turbomachine

Patent metadata

Field	Value
Publication number	US-9926976-B2
Application number	US-201314429804-A
Country	US
Kind code	B2
Filing date	Sep 19, 2013
Priority date	Sep 20, 2012
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

A thrust bearing comprises an electromagnetic stator with a stator surface and a rotor disk with a rotor surface facing the stator surface. The rotor disk comprises a radially inner portion made of a first material directly and exclusively connected to a radially outer portion made of a second material. The first material is a corrosion resistant metal or metal alloy and the second material is a ferromagnetic metal or metal alloy.

First claim

What is claimed is:

1. A thrust bearing, comprising:
an electromagnetic stator comprising a stator surface; and
a rotor disk rotatable relative to the electromagnetic stator and comprising a rotor surface facing the stator surface,
wherein the rotor disk comprises a radially inner portion made of a first material directly and exclusively connected to a radially outer portion made of a second material,
the first material is a corrosion resistant metal or metal alloy,
the second material is a ferromagnetic metal or metal alloy
the radially outer portion comprises a protective layer, coating, or cladding made of a corrosion resistant material, and
the protective layer, coating, or cladding extends from the radially outer portion beyond an interface between the radially outer portion and the radially inner portion.

2. The thrust bearing of claim 1 , wherein the radially inner portion is disk shaped and the radially outer portion is ring shaped, and wherein the outer portion is radially adjacent to the inner portion.

3. The thrust bearing of claim 2 , wherein the radially outer portion is welded to the radially inner portion.

4. The thrust bearing of claim 1 , wherein the radially outer portion is welded to the radially inner portion.

5. The thrust bearing of claim 1 , wherein the protective layer, coating or cladding is made of the first material.

6. A turbo machine, comprising:
a machine stator;
a machine rotor rotatable relative to the machine stator;
a thrust bearing disposed between the machine stator and the machine rotor, the thrust bearing comprising:
an electromagnetic stator having a stator surface, and
a rotor disk rotatable relative to the electromagnetic stator and having a rotor surface facing the stator surface;
wherein the rotor disk comprises a radially inner portion made of a first material directly and exclusively connected to a radially outer portion made of a second material;
the first material is a corrosion resistant metal or metal alloy, and
the second material is a ferromagnetic metal or metal alloy
the radially outer portion comprises a protective layer, coating, or cladding made of a corrosion resistant material, and
the protective layer, coating, or cladding extends from the radially outer portion beyond an interface between the radially outer portion and the radially inner portion.

7. The turbo machine of claim 6 , wherein the radially inner portion is axially adjacent to a shaft of the machine rotor at least on one side.

8. The turbo machine of claim 6 , wherein the radially inner portion and the machine rotor shaft have substantially the same axial cross-section.

9. The turbo machine of claim 6 , wherein the radially inner portion is disk shaped and the radially outer portion is ring shaped, and wherein the outer portion is radially adjacent to the inner portion.

10. The turbo machine of claim 6 , wherein the radially outer portion is welded to the radially inner portion.

11. The turbo machine of claim 6 , wherein the radially inner portion is axially adjacent to a shaft of the machine rotor on both sides.

12. A method of making a bearing rotor disk for an electromagnetic thrust bearing in a turbo machine, the method comprising:
forming a radially inner portion of the bearing rotor disk from a corrosion resistant metal or metal alloy;
forming a radially outer portion of the bearing rotor disk from a ferromagnetic metal or metal alloy;
connecting the radially inner portion directly to the radially outer portion; and
disposing a protective layer, coating, or cladding on the radially outer portion such that the protective layer, coating, or cladding extends from the radially outer portion beyond an interface between the radially outer portion and the radially inner portion, the protective layer, coating, or cladding being made of a corrosion resistant material.

13. The method of claim 12 , wherein the radially outer portion is welded to the radially inner portion.

14. The method of claim 12 , further comprising forming a thrust collar made of the corrosion resistant material to the radially inner ring portion for engagement with a rotor shaft of the turbo machine.

15. The turbo machine of claim 12 , wherein the protective layer, coating, or cladding is made of the first material.

Assignees

• Nuovo Pignone Srl

Inventors

• Masala Andrea
• Giorni Eugenio
• Camatti Massimo
• Bellacci Michelangelo

Classifications

• F16C2360/24

  Turbochargers · CPC title

• F16C2300/42

  corrosive, i.e. with aggressive media or harsh conditions · CPC title

• F16C32/0468

  of moving parts of the magnetic circuit, e.g. of the rotor · CPC title

• F05B2260/95

  Preventing corrosion · CPC title

• F16C32/0476 Primary

  with active support of one degree of freedom, e.g. axial magnetic bearings · CPC title