Damping system for a turbomachine slip ring

Patent metadata

Field	Value
Publication number	US-9657591-B2
Application number	US-201414501263-A
Country	US
Kind code	B2
Filing date	Sep 30, 2014
Priority date	Sep 30, 2014
Publication date	May 23, 2017
Grant date	May 23, 2017

Abstract

A damping system for a turbomachine slip ring includes a slip ring assembly. The slip ring assembly includes a rotating component which is coupled at one end to a rotor shaft of the turbomachine and a stator component which circumferentially surrounds a rotatable center core portion of the rotating component. The system further includes a static structure which defines a carrier sleeve where the carrier sleeve circumferentially surrounds a portion of the stator component. The system also includes a damping material which extends radially between an inner surface of the carrier sleeve and an outer surface of the stator component so as to dissipate vibrational energy of the slip ring assembly during rotation of the rotor shaft.

First claim

What is claimed is:

1. A damping system for a turbomachine slip ring, comprising:
a slip ring assembly including a rotating component coupled at one end to a rotor shaft of the turbomachine and a stator component circumferentially surrounding a rotatable center core portion of the rotating component, wherein the stator component is axially spaced from the coupled end of the rotating component;
a static structure including a carrier sleeve, the carrier sleeve circumferentially surrounding a portion of the stator component; and
a damping material, the damping material extending radially between an inner surface of the carrier sleeve and an outer surface of the stator component, wherein the damping material dissipates vibrational energy of the slip ring assembly during rotation of the rotor shaft.

2. The system as in claim 1 , wherein the damping material comprises a wire-mesh material.

3. The system as in claim 2 , wherein the wire-mesh material is a knitted wire mesh material.

4. The system as in claim 1 , wherein the carrier sleeve is configured to allow axial movement of the stator component during operation of the turbomachine.

5. The system as in claim 1 , wherein the portion of the stator component surrounded by the carrier sleeve includes an axially extending shaft fixed to an outer body of the stator component.

6. The system as in claim 1 , wherein the shaft is cylindrical.

7. The system as in claim 1 , wherein the static structure includes multiple struts which extend radially outwardly from the carrier sleeve and connect to an outer shroud.

8. The system as in claim 1 , wherein the static structure is vibrationally isolated from the turbomachine rotor shaft.

9. The system as in claim 7 , wherein the static structure is coupled to a bearing oil supply conduit.

10. A turbomachine, comprising:
a rotor shaft which extends along an axial centerline of the turbomachine;
a slip ring assembly including a rotating component coupled at one end to a corresponding end of the rotor shaft and a stator component circumferentially surrounding a rotatable center core portion of the rotating component, wherein the stator component is axially spaced from the coupled end of the rotating component;
a static structure including a carrier sleeve, the carrier sleeve circumferentially surrounding a portion of the stator component, wherein the static structure is vibrationally isolated from the turbomachine rotor shaft; and
a damping material, the damping material extending radially between an inner surface of the carrier sleeve and an outer surface of the stator component, wherein the damping material dissipates vibrational energy of the slip ring assembly during rotation of the rotor shaft.

11. The turbomachine as in claim 10 , wherein the damping material comprises a wire-mesh material.

12. The turbomachine as in claim 11 , wherein the wire-mesh material is a knitted wire mesh material.

13. The turbomachine as in claim 10 , wherein the carrier sleeve is configured to allow axial movement of the stator component during operation of the turbomachine.

14. The turbomachine as in claim 10 , wherein the portion of the stator component surrounded by the carrier sleeve includes an axially extending shaft fixed to an outer body of the stator component.

15. The turbomachine as in claim 10 , wherein the static structure includes multiple struts which extend radially outwardly from the carrier sleeve and connect to an outer shroud.

16. A gas turbine, comprising:
a compressor, a combustion section disposed downstream from the compressor, a turbine disposed downstream from the combustion section and a rotor shaft which extends through the compressor, combustion section and the turbine along an axial centerline of the gas turbine;
a slip ring assembly including a rotating component coupled at one end to a corresponding end of the rotor shaft and a stator component circumferentially surrounding a rotatable center core portion of the rotating component, wherein the center core portion is electronically coupled to one or more sensors disposed within the gas turbine and the stator component is electronically connected to a data acquisition unit, wherein the stator component is axially spaced from the coupled end of the rotating component;
a static structure defining a carrier sleeve, the carrier sleeve circumferentially surrounding a portion of the stator component, wherein the static structure is vibrationally isolated from the gas turbine rotor shaft; and
a damping material, the damping material extending radially between an inner surface of the carrier sleeve and an outer surface of the stator component, wherein the damping material dissipates vibrational energy of the slip ring assembly during rotation of the rotor shaft.

17. The gas turbine as in claim 16 , wherein the damping material comprises a wire-mesh material.

18. The gas turbine as in claim 17 , wherein the wire-mesh material is a knitted wire mesh material.

19. The gas turbine as in claim 16 , wherein the portion of the stator component surrounded by the carrier sleeve includes an axially extending shaft fixed to an outer body of the stator component.

20. The gas turbine as in claim 16 , wherein the static structure includes multiple struts which extend radially outwardly from the carrier sleeve and connect to an outer shroud.

Assignees

• Gen Electric

Inventors

• Schleif Kurt Kramer
• Shaw Donald W
• Snider Zachary John

Classifications

• F05D2270/80

  Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges · CPC title

• F01D21/003

  Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title

• F01D25/04 Primary

  Antivibration arrangements · CPC title