IP Library Granted Patent US 8,397,384
Granted Patent B2
US 8,397,384 · App. 12/265,969 · Granted Mar 19, 2013

Method for attaching a bearing supporting a rotor on a turbomachine

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Quick Facts
Patent No.
US 8,397,384
App. No.
12/265,969
Granted
Mar 19, 2013
Kind
B2
Abstract

A method for attaching a bearing on a turbomachine including a stator and a rotor, the bearing including: a first portion attached on the stator of the turbomachine by a plurality of screws and nuts, a second portion attached on the rotor, rotationally movable in one given rotation direction, and a rolling bearing provided between the first and second portions of the bearing is disclosed. The method provides using screws having a screwing rotation direction contrary to the rotation direction of the rotor.

Claims (10)

1. A method for attaching a bearing on a turbomachine comprising a stator and a rotor, the bearing including:

a first portion attached on the stator of the turbomachine by a plurality of screws and nuts,

a second portion attached on the rotor of the turbomachine, rotationally movable in one given rotation direction,

and a rolling bearing provided between the first and second portions of the bearing,

wherein said method includes using the plurality of screws each having a screwing rotation direction contrary to the rotation direction of the rotor.

2. The method for attaching a bearing on a turbomachine according to claim 1 , wherein, when the rotor rotation direction goes clockwise as seen from behind the turbomachine, a head of each screw is located downstream and the corresponding nut is located upstream, and the screws used are left-hand screws.

3. The method for attaching a bearing on a turbomachine according to claim 1 , wherein, when the rotor rotation direction goes clockwise as seen from behind the turbomachine, a head of each screw is located upstream and the corresponding nut is located downstream, and the screws used are right-hand screws.

4. The method for attaching a bearing on a turbomachine according to claim 1 , wherein, when the rotor rotation direction goes counter clockwise as seen from behind the turbomachine, a head of each screw is located downstream and the corresponding nut is located upstream, and the screws used are right-hand screws.

5. The method for attaching a bearing on a turbomachine according to claim 1 , wherein, when the rotor rotation direction goes counter clockwise as seen from behind the turbomachine, a head of each screw is located upstream and the corresponding nut is located downstream, and the screws used are left-hand screws.

6. The method for attaching a bearing on a turbomachine according to any of the preceding claims, wherein the first portion of the bearing comprises a first flange and the stator of the turbomachine comprises a second flange, the first and second flanges being clamped against each other and having respective circular ports with screws therethrough.

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 Nov 7, 2008
From: GIRARD, MANUEL CLAUDE BERTRAND; TRIBOUILLER, JEROME
To: SNECMA
Reel/Frame 021801/0140 →