IP Library Patent Application 14343658
Patent Application
App. No. 14/343,658

PINION VIBRATION DAMPING USING VISCOELASTIC PATCH

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Quick Facts
Patent No.
US None
App. No.
14/343,658
Abstract

A gearwheel extending in an axial direction and in a radial direction, the gearwheel including a radial web carrying an axial annular rim, the rim carrying gear teeth. The web includes a vibration damper device including a layer of viscoelastic material and a backing layer. The layer of viscoelastic material is arranged axially between the radial web and the backing layer, and the layer of viscoelastic material is fixed directly to the web.

Claims (13)

1 - 9 . (canceled)

10 : A gearwheel extending in an axial direction and in a radial direction, the gearwheel comprising:

a radial web carrying an axial annular rim, the rim carrying gear teeth;

wherein the web includes a vibration damper device including a layer of viscoelastic material and a backing layer, the layer of viscoelastic material being arranged axially between the radial web and the backing layer, and the layer of viscoelastic material being fixed directly to the web, and

wherein the radial web is substantially frustoconical in shape, the vibration damper device being placed on an inner side of the frustoconical shape.

11 : A gearwheel according to claim 10 , wherein the vibration damper device is in a form of a ring that is continuous, split, or in multiple segments.

12 : A gearwheel according to claim 10 , wherein the backing layer presents a radial length that is at least equal to a length of the layer of viscoelastic material.

13 : A gearwheel according to claim 10 , wherein the layer of viscoelastic material presents an axial thickness in a range of 0.1 mm to 3 mm.

14 : A gearwheel according to claim 10 , wherein the backing layer presents an axial thickness in a range of 0.5 mm to 2 mm.

15 : A gearwheel according to claim 10 , further comprising a hub, and wherein the vibration damper device is arranged closer to the annular rim than to the hub.

16 : A turbine engine comprising a gearwheel according to claim 10 , wherein the gearwheel is a pinion.

17 : A method of fabricating a gearwheel according to claim 10 , comprising vulcanizing the layer of viscoelastic material on the radial web.

18 : A method of fabricating a gearwheel according to claim 10 , comprising adhesively bonding the layer of viscoelastic material on the radial web.

Assignments (2)
CHANGE OF NAME Recorded May 11, 2018
From: TURBOMECA
To: SAFRAN HELICOPTER ENGINES
Reel/Frame 046127/0021 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 7, 2014
From: MARSAUDON, MATHIEU; CUTULI, PHILIPPE
To: TURBOMECA
Reel/Frame 032381/0213 →