Vibration damper assembly for the buckets of a turbine

• US 6,851,932 B2
• Filed: 05/13/2003
• Issued: 02/08/2005
• Est. Priority Date: 05/13/2003
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Wassynger, Stephen Paul, Lagrange, Benjamin Arnette, Worley, Kevin Lee
• Primary Examiner(s): Nguyen, Hoang
• Application Number:
  US10/436,202
• Publication Number:
  US 20040228731A1
• Time in Patent Office: 637 Days
• Field of Search: 416/190, 416/193.A, 416/500, 416/219.R
• US Class Current: 416/190
• CPC Class Codes: F01D 5/22 Blade-to-blade connections, e.g. for damping vibrations
• CPC Class Codes: F01D 5/26 Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
• CPC Class Codes: F05D 2260/96 Preventing, counteracting or reducing vibration or noise
• CPC Class Codes: Y10S 416/50 Vibration damping features

Abstract

A damper pin is disposed between adjacent buckets of a turbine rotor. A first bucket has circumferentially extending supports defining a pair of axially spaced surfaces on which a damper pin rests in a cold condition of the turbine. The adjacent bucket is undercut adjacent its platform to provide an angled surface overlying a generally correspondingly angled surface of the damper pin. The damper pin fits slightly loose within the recess and, upon turbine rotation at speed, the angled surfaces of the damper pin and recess cooperate to bias the damper pin against the first bucket whereby the damper pin engages both buckets and dissipates vibratory action.

Claims

1. An assembly of buckets for a turbine wheel, comprising:

a pair of circumferentially adjacent buckets each having a bucket airfoil, a platform, a shank and a dovetail, the dovetails being shaped for securement of the buckets to the turbine wheel;

a first bucket of said pair of buckets including at least a first support extending in a generally circumferential direction from a side thereof and beyond a marginal edge of the platform of said first bucket, said support including a support surface;

a second bucket of said pair thereof having an undercut opening in a generally circumferential direction toward said first bucket and underlying the platform of said second bucket, said undercut including a surface angled radially outwardly and toward said first bucket, said first bucket including a generally radially extending surface adjacent said support, said radially extending surface and said support surface of said first bucket, together with the angled surface of said undercut of said second bucket, forming a recess between said pair of buckets underlying said second bucket; and

a damper pin disposed between said adjacent buckets and in said recess, said damper pin being movable within said recess between a first position resting on said support surface and a second position engaging said radially extending surface of said first bucket and said angled surface of the recess of said second bucket for dissipating vibratory motion of the buckets.

2. An assembly according to claim 1 wherein said damper pin and said recess are sized to enable a third surface of the damper pin to lift off said support surface in response to rotation of the turbine wheel.

3. An assembly according to claim 1 including a second support on said first bucket generally axially spaced from said first support and having a second support surface for supporting the damper pin, at least one boss along the damper pin being disposed between said supports for preventing displacement of said damper pin in at least one axial direction.

4. An assembly according to claim 1 including a second support generally axially spaced from said first support on said first bucket and having a second support surface for supporting said damper pin, and a pair of bosses along said damper pin disposed between said support surfaces for preventing displacement of said damper pin in opposite axial directions.

5. An assembly according to claim 1 wherein said recess opens along common axial faces of said buckets, exposing an end of the damper pin for viewing from an axial direction and externally of the buckets and wheel.

6. An assembly according to claim 1 wherein said damper pin and said recess are generally triangularly-shaped and have respective registering surfaces configured relative to one another to preclude rotation of the damper pin about an axis thereof generally parallel to an axis of rotation of the turbine wheel.

7. An assembly according to claim 1 wherein the surfaces of said first and second buckets defining said recess are machined surfaces.

8. An assembly according to claim 1 wherein said recess along said second bucket lies on the side of said bucket corresponding to a pressure surface of the bucket airfoil.

9. An assembly according to claim 1 wherein said support projects from a side of said first bucket corresponding to a suction side of the airfoil of said first bucket.

15. An assembly according to claim 9 wherein said recess along said second bucket lies on the side of said bucket corresponding to a pressure surface of the bucket airfoil.

16. An assembly according to claim 9 wherein said support projects from a side of said first bucket corresponding to a suction side of the airfoil of said first bucket.

10. An assembly of buckets for a turbine wheel, comprising:

a pair of circumferentially adjacent buckets each having a bucket airfoil, a platform, a shank and a dovetail, the dovetails being shaped for securement of the buckets to the turbine wheel;

a first bucket of said pair of buckets including first and second supports extending in a generally circumferential direction from a side thereof and beyond a marginal edge of the platform of said first bucket, said supports including first and second support surfaces;

a second bucket of said pair thereof having an undercut opening in a generally circumferential direction toward said first bucket and underlying the platform of said second bucket, said undercut including a surface angled radially outwardly and toward said first bucket, said first bucket including a contact surface, said contact surface and said support surface of said first bucket, together with the angled surface of said undercut of said second bucket, forming a recess between said pair of buckets underlying said second bucket; and

a damper pin disposed between said adjacent buckets and in said recess, at least one boss along the damper pin disposed between said supports for preventing displacement of said damper pin in opposite axial directions, said damper pin being movable within said recess between a first position resting on said support surface and a second position engaging said contact surface of said first bucket and said angled surface of the recess of said second bucket for dissipating vibratory motion of the buckets.

11. An assembly according to claim 10 wherein said damper pin and said recess are sized to enable a third surface of the damper pin to lift off said support surfaces in response to rotation of the turbine wheel.

12. An assembly according to claim 10 wherein said recess opens along common axial faces of said buckets, exposing an end of the damper pin for viewing from an axial direction and externally of the buckets and wheel.

13. An assembly according to claim 10 wherein said damper pin and said recess are generally triangularly-shaped and have respective registering surfaces configured relative to one another to preclude rotation of the damper pin about an axis thereof generally parallel to an axis of rotation of the turbine wheel.

14. An assembly according to claim 10 wherein the surfaces of said first and second buckets defining said recess are machined surfaces.