Vibration damping

• US 6,659,725 B2
• Filed: 03/28/2002
• Issued: 12/09/2003
• Est. Priority Date: 04/10/2001
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Yeo, Stuart, Goodman, Peter J
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): Kershteyn, Igor
• Application Number:
  US10/107,153
• Publication Number:
  US 20020146322A1
• Time in Patent Office: 621 Days
• Field of Search: 416/500, 416/190
• 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: Y10S 416/50 Vibration damping features

Abstract

A vibration damper 46 for a gas turbine engine has convergent friction surfaces 48a and 48b and is located radially inward of the platforms 20a and 20b of two adjacent turbine blades. The angle subtended by the friction surfaces 48a and 48b is smaller than that subtended by the angled faces 22a and 22b associated with the platforms 20a and 20b. The center of mass of the damper 46 lies in a plane bisecting the angle subtended by the friction surfaces 48a and 48b. In use the damper 46 is urged radially outwards by centrifugal force so that at least one of the friction surfaces 48a and 48b makes planar contact with at least one of the angled faces 22a and 22b. Vibrational energy is dissipated by the resultant sliding movement between the friction surfaces 48a and 48b and the angled faces 22a and 22b. A secondary vibration damping mechanism arises from the oscillation of the damper 46 between the platforms 20a and 20b.

Claims

1. A vibration damper for installation between a first blade of a gas turbine engine and a second blade of a gas turbine engine, the second blade being circumferentially adjacent to the first blade, the first blade having associated with it a first, planar face, the second blade having associated with it a second, planar face, the first face and the second face being radially convergent, the damper having associated with it a first, planar friction surface for contacting the first face and a second, planar friction surface for contacting the second face, the first friction surface and the second friction surface being radially convergent, the closest-spaced ends of the first friction surface and the second friction surface being spaced apart by a distance at least as great as the maximum circumferential gap between the radially outer ends of the first face and the second face, the angle subtended by the first friction surface and the second friction surface being smaller than the angle subtended by the first face and the second face;

wherein the mass of the damper is disposed such that the centre of mass of said damper lies in a plane bisecting the angle subtended by said first friction surface and said second friction surface.

2. A damper according to claim 1, wherein said damper is substantially wedge-shaped in cross section.

3. A damper according to claim 1, wherein said closest-spaced ends of said first friction surface and said second friction surface are joined by a convex, curved surface.

4. A damper according to claim 1, wherein the difference between the angle subtended by said first friction surface and said second friction surface and the angle subtended by said first face and said second face is approximately 10°

.

5. A damper according to claim 1, wherein the angle subtended by said first friction surface and said second friction surface is approximately 110°

.

6. A damper according to claim 1, wherein the angle subtended by said first face and said second face is approximately 120°

.