IP Library Granted Patent US 7,404,678
Granted Patent B2
US 7,404,678 · App. 10/517,763 · Granted Jul 29, 2008

Rotor recentering after decoupling

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Quick Facts
Patent No.
US 7,404,678
App. No.
10/517,763
Granted
Jul 29, 2008
Kind
B2
Abstract

A recentering device for a rotor shaft for recentering a rotor shaft relative to an axis X of a stator structure in the event of decoupling caused by excessive imbalance. The shaft, in normal operating conditions, lies on the axis X and is radially supported by a bearing support disposed in a bore of the axis X in the stator structure. The bearing support has an outside diameter smaller than the diameter of the bore, to enable the bearing support to orbit about the axis X in the event of decoupling. The bearing support is connected to the stator structure by radially fusible elements. The recentering device recenters the bearing support after decoupling.

Claims (15)

1. A recentering device for a rotor shaft for recentering a rotor shaft relative to an axis X of a stator structure in an event of a decoupling caused by excessive imbalance, said shaft, in an absence of said decoupling, lying on the axis X and being radially supported by a bearing support disposed in a bore of the axis X in said stator structure, said bearing support having an outside diameter that is smaller than a diameter of said bore, to enable said bearing support to orbit about the axis X in the event of said decoupling, said bearing support being connected to the stator structure by radially fusible elements, said device comprising:

means for recentering the bearing support after said decoupling,

wherein the recentering means of the bearing support comprises means for generating a movement in precession by said bearing support in a direction contrary to a direction of said bearing support's orbits traveled after said decoupling, and a plurality of devices for decreasing permitted clearance of said bearing support relative to the axis X, said devices for decreasing permitted clearance being arranged regularly around the axes of two parts constituted by the stator structure and the bearing support, and each part including a first ramp provided on one of said two parts and a protuberance provided on the other of said two parts, said protuberance being, in the absence of said decoupling, radially spaced apart apart from said first ramp and configured to come into contact with said first ramp during the movement in precession of said bearing support.

2. A device according to claim 1 , wherein all the protuberances are configured to be in contact with the first ramps at a same time.

3. A device according to claim 1 , wherein each first ramp has a profile of an involute to a circle, and two adjacent first ramps are connected by a radial shoulder.

4. A device according to claim 3 , wherein each first ramp has a profile of an Archimedes spiral.

5. A device according to claim 1 , wherein the protuberances are made in a form of blocks.

6. A device according to claim 1 , wherein each protuberance is formed by an end portion of a second ramp, said second ramp having a second profile similar to a first profile of an associated first ramp.

7. A device according to claim 6 , wherein each first ramp is made of elastomer and the second ramp is made of metal and can roll on the first ramp, without sliding, after said decoupling, to generate the movement in precession.

8. A device according to claim 1 , wherein each first ramp and the protuberance are made of metal.

9. A device according to claim 8 , wherein each protuberance is located, in the absence of said decoupling, in a position radially spaced apart from an associated first ramp by a distance that is greater than an expected radial displacement of the bearing support during said decoupling.

10. A device according to claim 1 , wherein the means for generating the movement in precession comprises an elastomer ring secured to the stator structure, said elastomer ring surrounding the bearing support and being in permanent contact therewith so that the bearing support can roll without sliding in the bore of said elastomer ring after said decoupling.

11. A device according to claim 10 , wherein said elastomer ring is disposed in the bore of the stator structure.

12. A device according to claim 10 , wherein said elastomer ring is rigid and is connected to the stator structure by a flexible metal support.

13. A device according to claim 1 , comprising three first ramps and three protuberances.

Assignments (4)
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 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 18, 2005
From: PLONA, DANIEL
To: SNECMA MOTEURS
Reel/Frame 016287/0875 →