IP Library Granted Patent US 8,136,999
Granted Patent B2
US 8,136,999 · App. 12/357,045 · Granted Mar 20, 2012

Turbomachine shaft guidance

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Quick Facts
Patent No.
US 8,136,999
App. No.
12/357,045
Granted
Mar 20, 2012
Kind
B2
Abstract

A support for a bearing that guides a shaft in a turbomachine is disclosed. The support includes an annular part made of a shape memory material which retains an initial shape when the load applied to it remains below a threshold value and which deforms, absorbing energy when the applied load becomes at least equal to the threshold value. The annular part is capable of reverting at least approximately to its initial shape when the applied load drops back below the threshold value.

Claims (11)

1. A support for a bearing that guides a shaft in a turbomachine, the support comprising:

an annular part made of a shape memory material which retains an initial shape when the load applied to it remains below a threshold value and which deforms, absorbing energy when the applied load becomes at least equal to the threshold value, this annular part being capable of reverting at least approximately to its initial shape when the applied load drops back below the threshold value; and

controlled means of heating the shape memory annular part to cause this annular part to revert to its initial shape when the applied load is below the threshold value.

2. A bearing support according to claim 1 , wherein the heating means comprise means of conveying hot air onto the shape memory annular part.

3. A bearing support according to claim 2 , further comprising means of guiding hot air onto the shape memory annular part.

4. A bearing support according to claim 3 , wherein the guide means comprise a sheet metal deflector mounted around the shape memory annular part.

5. A bearing support according to claim 1 , wherein the shape memory annular part connects upstream and downstream ends of the support together.

6. A bearing support according to claim 1 , wherein the shape memory annular part comprises thin longitudinal blades uniformly distributed about the axis of the turbomachine.

7. A bearing support according to claim 6 , wherein the ends of the thin blades are brazed or welded to the end parts of the support.

8. A bearing support according to claim 1 , further comprising an annular sealing envelope positioned radially on the inside of the shape memory annular part.

9. A turbomachine comprising a shaft guided in upstream and downstream bearings which are supported by supports that are fixed to a casing, wherein at least one of the supports is a bearing support according to claim 1 .

Assignments (2)
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 →