IP Library Granted Patent US 8,209,834
Granted Patent B2
US 8,209,834 · App. 12/354,222 · Granted Jul 3, 2012

Centering a part inside a shaft

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Quick Facts
Patent No.
US 8,209,834
App. No.
12/354,222
Granted
Jul 3, 2012
Kind
B2
Abstract

A device for centering a tube inside a hollow shaft is disclosed. The device includes a deformable device interposed between the tube and the hollow shaft and including bearing members for bearing against the inside surface of the shaft and suitable for being spaced away from the inside surface of the shaft in order to enable them to be moved inside the shaft. The deformable device is made of a shape-memory material suitable for deforming to press the bearing members against the inside surface of the shaft or to space them away therefrom on being subjected to a predetermined temperature.

Claims (10)

1. A device for centering a part inside a hollow shaft in a turbomachine, the device comprising:

radially deformable means interposed between the part and the hollow shaft and including bearing members for bearing against an inside surface of the shaft, the bearing members being suitable for being spaced away from the inside surface of the shaft to enable them to be moved inside the shaft,

wherein the deformable means are made at least in part out of a shape-memory material suitable for radially pressing the bearing members against the inside surface of the shaft, or for radially spacing the bearing members away therefrom when the material is subjected to a predetermined temperature,

wherein the part is a tube, and

wherein the deformable means comprise rods of shape-memory material, each having a radially inner end fastened to an outside surface of the tube and a radially outer end carrying a bearing shoe for bearing against the inside surface of the shaft, the radially outer end of each rod being suitable for curving radially inwards by deformation of the shape-memory material in order to move the corresponding bearing shoe away from the inside surface of the shaft.

2. The device according to claim 1 , wherein the deformable means are initially shaped into a position for bearing against the shaft at a temperature higher than a transition temperature T t of the shape-memory material, and are then retracted under mechanical stress at a temperature lower than the transition temperature T t , so as to be capable subsequently, by a single shape-memory effect, of pressing the bearing members against the shaft by deformation of the shape-memory material when it is heated to a temperature higher than the transition temperature T t .

3. The device according to claim 2 , wherein the transition temperature T t of the shape-memory material is higher than 100° C.

4. A device according to claim 1 , wherein the deformable means are initially subjected to thermomechanical cycles in which they are shaped in turn in a deployment position at a temperature higher than a transition temperature T t of the shape-memory material and then in a retraction position at a temperature that is lower than the transition temperature T t , so as to be subsequently suitable for pressing the bearing members against the hollow shaft by the shape-memory material deforming on being heated to a temperature higher than the transition temperature T t , and for retracting the bearing members by the shape-memory material deforming on being cooled to a temperature lower than the transition temperature T t .

5. The device according to claim 1 , wherein each bearing shoe is in the form of a ring sector suitable for matching the shape of the inside surface of the shaft when in the deployed position, with the set of bearing shoes, when in the retracted position, forming a substantially continuous ring surrounding the tube.

6. A turbomachine including at least one centering device of the type described in claim 1 .

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 Mar 25, 2009
From: MONS, CLAUDE MARCEL; RABERIN, LAURENT; RONGVAUX, JEAN-MARC; ROUSSELIN, STEPHANE
To: SNECMA
Reel/Frame 022447/0841 →