IP Library Granted Patent US 8,721,256
Granted Patent B2
US 8,721,256 · App. 13/021,299 · Granted May 13, 2014

Turbomachine optimized for fastening a rotary shaft bearing, A method of mounting said bearing on said turbomachine

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Quick Facts
Patent No.
US 8,721,256
App. No.
13/021,299
Granted
May 13, 2014
Kind
B2
Abstract

A turbomachine including a shaft, a bearing for supporting the shaft and including an outer ring, and a support for the bearing, the support having a flange to which the outer ring is fastened by fasteners, is provided. Each fastener includes a fastener bolt and a nut screwed together. The turbomachine further includes, for each fastener, a position-retention device for retaining the bolt, and suitable for retaining the bolt in a position that is stationary relative to the bearing support or the outer ring, even in the absence of the nut. The head of the fastener bolt and the position-retention device may be of small dimensions, thereby enabling the fastening of the flange to the bearing support to be optimized, and in particular enabling the weight of the fastening to be optimized. A method of mounting the bearing of the turbomachine is also provided.

Claims (21)

1. A turbomachine comprising:

a rotary shaft;

a shaft support bearing including an outer ring;

a support for said bearing having a flange:

a plurality of bolt fasteners which fastens the flange of the support to the outer ring, each fastener comprising first and second portions that are screwed together; and

for each fastener position-retention means for retaining a first portion of the fastener in position and suitable for retaining the fastener substantially in a stationary position relative to the bearing support, even in the absence of the second fastener portion,

wherein said first portion comprises a fastener bolt and the second portion being a nut, and

wherein said fastener position-retention means includes a fixing bolt, and a head of the fastener bolt presenting a passage that is offset from an axis of the fastener bolt and through which said fixing bolt passes.

2. A turbomachine according to claim 1 , wherein the bearing support includes spokes and said at least one fastener is located between the spokes.

3. A turbomachine according to claim 1 , wherein said fixing bolt is fastened to the bearing support and retains the fastener bolt thereon before the nut is screwed onto the fastener bolt.

4. A turbomachine according to claim 3 , wherein said fixing bolt enables the fastener bolt to be held in a desired angular position while the nut is being screwed on.

5. A turbomachine according to claim 3 , wherein said fixing bolt comprises a single fixing rod penetrating in the bearing support or a part secured thereto, through a head of the fastener bolt.

6. A turbomachine according to claim 5 , wherein the head of the fastener bolt is flat and presents a hole on one side relative to the axis of the fastener bolt for the purpose of passing the fixing rod of a said fixing bolt.

7. A turbomachine according to claim 5 , wherein the fixing rod passes through the hole in the head of the fastener bolt with clearance.

8. A turbomachine according to claim 1 , wherein a head of the fastener bolt is prevented from turning by a surface of the bearing support.

9. A turbomachine according to claim 1 , wherein the head of the fastener bolt is flat and extends in a plane perpendicular to the axis of the fastener bolt, and a shank of the fastener bolt extends from the head of the fastener bolt along the axis of the fastener bolt.

10. A method of mounting a bearing on a bearing support placed around a rotary shaft of a turbomachine, said bearing including an outer ring, said method comprising:

fixing a plurality of fastener bolts to the bearing support using position-retention means that retain said bolts in a position that is substantially stationary relative to the bearing support, even in the absence of nuts, wherein said fastener bolts are fixed using a plurality of fixing bolts, each fixing bolt being fixed to the bearing support and retaining a fastener bolt on the bearing support before a nut is screwed onto said bolt, and wherein a head of each of said fastener bolts presents a passage that is offset from an axis of the fastener bolt and through which one of said fixing bolts passes;

positioning the outer ring on a flange of the bearing support; and

fastening the outer ring to the flange by screwing a plurality of nuts on said fastener bolts.

11. A method according to claim 10 , wherein the head of the fastener bolt is flat and extends in a plane perpendicular to the axis of the fastener bolt, and a shank of the fastener bolt extends from the head of the fastener bolt along the axis of the fastener bolt.

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 Feb 7, 2011
From: SERVANT, REGIS EUGENE HENRI
To: SNECMA
Reel/Frame 025750/0296 →