IP Library Granted Patent US 10,316,676
Granted Patent B2
US 10,316,676 · App. 14/760,894 · Granted Jun 11, 2019

Device for sealing between the coaxial shafts of a turbomachine

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Quick Facts
Patent No.
US 10,316,676
App. No.
14/760,894
Granted
Jun 11, 2019
Kind
B2
Abstract

A sealing device for sealing between coaxial shafts of a turbomachine, the sealing device including an elastic ring having a circular central opening allowing a sliding connection with an internal shaft, an external surface configured to engage with an internal surface of a portion of an external shaft, two retaining components situated one on either side of the elastic ring and allowing the elastic ring an axial clearance, wherein the elastic ring is a profile section.

Claims (14)

1. A sealing device for sealing between rotating coaxial shafts of a turbomachine, said sealing device comprising:

an elastic ring having:

a circular central opening allowing a sliding connection with an internal shaft,

an external surface configured to engage with an internal surface of a portion of an external shaft, and

two metal plates situated one on either side of said elastic ring and allowing said elastic ring an axial clearance,

wherein the elastic ring is a profile section and wherein the external surface of the elastic ring has a shape that is configured to prevent a rotation of the elastic ring with respect to the external shaft, and wherein the external surface of the elastic ring is of oval cross section.

2. The sealing device according to claim 1 , wherein the external surface of the elastic ring is of elliptical cross section.

3. The sealing device according to claim 1 , wherein the elastic ring comprises a slot allowing an angular opening of said elastic ring.

4. The sealing device according to claim 1 , wherein the shape of the external surface is such that the elastic ring and the external shaft are integral in accordance with a rotational movement around an axis of rotation of the external shaft.

5. The sealing device according to claim 1 , wherein the two metal plates are integral with the internal shaft.

6. A transmission assembly comprising:

an external shaft of a turbomachine comprising two coaxial shafts, including a portion of which an internal surface is of oval cross section, and

a sealing device according to claim 1 , said internal surface of the portion of the external shaft being configured to engage with the external surface of the elastic ring of the sealing device, and the external surface of the elastic ring is of oval cross section.

7. The transmission assembly according to claim 6 , wherein the internal surface of the external shaft is of elliptical cross section, and the external surface of the elastic ring is of elliptical cross section.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 14, 2015
From: BAPTISTA, JONATHAN BORIS
To: SNECMA
Reel/Frame 036081/0834 →