Variable vane damping assembly

Patent metadata

Field	Value
Publication number	US-9410443-B2
Application number	US-201213360002-A
Country	US
Kind code	B2
Filing date	Jan 27, 2012
Priority date	Jan 27, 2012
Publication date	Aug 9, 2016
Grant date	Aug 9, 2016

Abstract

A variable vane damping assembly includes an inner bushing and an outer bushing. The inner bushing comprises an elastomeric material.

First claim

We claim:

1. A variable vane damping assembly, comprising: an inner bushing that is bondable to a variable vane; and an outer bushing that is bondable to the inner bushing, wherein the inner bushing comprises an elastomeric material, wherein the inner bushing and the outer bushing are configured to rotate together with the variable vane, wherein the inner bushing and the outer bushing are both cylindrical, wherein the inner bushing and the outer bushing have a cylindrical cross-section, and the inner bushing and the outer bushing have a uniform diameter along an entire axial length of the inner bushing and the outer bushing and wherein the inner bushing is bonded to a trunnion of the variable vane.

2. The variable vane damping assembly of claim 1 , wherein the outer bushing comprises a metallic material.

3. The variable vane damping assembly of claim 1 , wherein an entirety of the inner bushing is molded, and the outer bushing and the variable vane hold the inner bushing during the molding.

4. The variable vane damping assembly of claim 1 , wherein the inner bushing comprises, exclusively, the elastomeric material.

5. The variable vane damping assembly of claim 1 , wherein the inner bushing is secured to the variable vane exclusively with the elastomeric material.

6. The variable vane damping assembly of claim 1 , wherein the inner bushing has a radially innermost facing surface, and the inner bushing is bondable to a variable vane along an entire axial length of the radially innermost facing surface.

7. A variable vane assembly, comprising: a trunnion of a variable vane; an elastomeric bushing bonded and secured to the trunnion with exclusively an elastomeric material; and an outer bushing bonded to the elastomeric bushing, the outer bushing being a cylindrical outer bushing, the outer bushing having a cylindrical cross-section, and the outer bushing having a uniform diameter along an entire axial length of an outer surface of the outer bushing.

8. The variable vane assembly of claim 7 , wherein the trunnion is at a radially inner end of the variable vane relative to a central axis of a turbomachine having the variable vane.

9. The variable vane assembly of claim 7 , wherein the trunnion is formed with the variable vane.

10. The variable vane assembly of claim 7 , wherein the outer bushing is metallic.

11. The variable vane assembly of claim 7 , wherein the elastomeric bushing is entirely comprised of the elastomeric material.

12. The variable vane assembly of claim 7 , wherein the elastomeric bushing has a radially innermost facing surface, and the elastomeric bushing is bonded to the variable vane along an entire axial length of the radially innermost facing surface.

13. The variable vane assembly of claim 7 , wherein the elastomeric bushing has a radially innermost facing surface extending from a first axial end of the elastomeric bushing to an opposite, second axial end of the elastomeric bushing, the elastomeric material providing the entire radially innermost facing surface.

14. A method of damping a variable vane, comprising: moving an elastomeric material together with a variable vane; positioning the elastomeric material within an outer bushing; and bonding the elastomeric material to the variable vane; and securing the outer bushing to the variable vane using, exclusively, the elastomeric material, wherein the outer bushing is a cylindrical outer bushing, the outer bushing having a cylindrical cross-section, and the outer bushing having a uniform diameter along an entire axial length of an outer surface of the outer bushing.

15. The method of claim 14 , including bonding the elastomeric material to the outer bushing.

16. The method of claim 14 , including molding the elastomeric material and holding the elastomeric material during the molding using the variable vane and the outer bushing.

17. The method of claim 14 , wherein the outer bushing has a first axial length, and the elastomeric material has a second axial length that is the same as the first axial length.

18. The method of claim 14 , wherein the variable vane has a trunnion with a radially outwardly facing surface that is contacted exclusively with the elastomeric material.

Assignees

• Dube David P
• Hayford Richard K
• United Technologies Corp

Inventors

• Dube David P
• Hayford Richard K

Classifications

• F05D2270/58

  by mechanical means, e.g. levers, gears or cams · CPC title

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F01D25/04

  Antivibration arrangements · CPC title

• F01D17/162 Primary

  for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F05D2300/501

  Elasticity · CPC title