IP Library Granted Patent US 9,482,271
Granted Patent B2
US 9,482,271 · App. 14/780,038 · Granted Nov 1, 2016

Disengageable axial thrust bearing with internal preload

Inventors: Sébastien Boufflert (Louviers, FR); Philippe Bourdin (Saint-just, FR); Alban Lemaitre (Vernon, FR); Fabien Tessier (Vernon, FR)
Assignee: SNECMA
F16C25/083F16C19/10F16C19/166F16C33/60F16C27/08F16C39/02
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,482,271
App. No.
14/780,038
Granted
Nov 1, 2016
Kind
B2
Abstract

In a disengageable axial thrust bearing for a rotary machine, an outer ring has first and second outer half-rings ( 114 A, 114 B) centered in a casing ( 116 ) and clamped in the axial direction between a stationary thrust member ( 118 ) and a first pre-loading system ( 120 ) exerting a first predetermined axial force such that, so long as the axial load exerted on the axial thrust bearing via a synchronization element ( 106 ) is greater than a determined threshold value, rolling elements ( 110 ) with oblique contacts present respective single lines ( 130 ) having two points of contact ( 130 A, 130 B) with an inner ring ( 102 ) and with the first outer half-ring ( 114 A), the second outer half-ring ( 114 B) being spaced apart from the first by a second predetermined axial force exerted by a second pre-loading system ( 126 ) inserted in the axial direction between the first and second outer half-rings, and such that the inner ring ( 102 ) is driven in rotation by the synchronization element, whereas, when the axial load exerted on the axial thrust bearing becomes less than this determined threshold value, a second line ( 132 ) having two additional points of contact ( 132 A, 132 B) is created between each of the oblique-contact rolling elements ( 110 ) and the inner ring ( 102 ) and the second outer half-ring ( 103 B) such that the axial thrust bearing is disengaged.

Claims (10)

1. A disengageable axial thrust bearing for a rotary machine, the thrust bearing comprising an inner ring arranged around a rotary shaft in radially non-interfering manner on said shaft, a synchronization element mounted on said rotary shaft to drive rotation of said inner ring selectively, an outer ring comprising first and second outer half-rings centered in a casing and clamped in the axial direction between firstly a stationary thrust member and secondly a first pre-loading system exerting a first predetermined axial force, and oblique-contact rolling elements, wherein the thrust bearing further comprises a second pre-loading system inserted in the axial direction between said first and second outer half-rings and exerting a second predetermined axial force less than the first predetermined axial force such that, so long as the axial load exerted on the axial thrust bearing via the synchronization element is greater than a determined threshold value, each of the rolling elements presents a single line with two points of contact respectively with the inner ring and with the first outer half-ring, the second outer half-ring being spaced apart from the first by the second predetermined axial force exerted by the second pre-loading system, and such that the inner ring is driven in rotation by said synchronization element, whereas, when the axial load exerted on the axial thrust bearing becomes less than this determined threshold value, a second line with two additional points of contact is created between each of the rolling elements and respectively the inner ring and the second outer half-ring such that the axial thrust bearing is disengaged, with rotation of the inner ring stopping as a result of inertia and friction internal to the thrust member via the four points of contact between each rolling element and the inner ring and the first and second outer half-rings.

2. A disengageable axial thrust bearing according to claim 1 , wherein the first and second pre-loading systems comprise respective resilient assemblies.

3. A disengageable axial thrust bearing according to claim 2 , wherein said resilient assembly comprises one or more spring washers.

4. A disengageable axial thrust bearing according to claim 1 , wherein the first pre-loading system exerts an axial force in the direction opposite to the axial load exerted on the axial thrust bearing via the synchronization element.

5. A disengageable axial thrust bearing according to claim 1 , wherein the second pre-loading system is held in position by an annular clip that is positioned in respective grooves associated in each of the outer half-rings.

6. A disengageable axial thrust bearing according to claim 1 , wherein the first outer half-ring providing a first line of points of contact includes a width that is greater than a width of the second outer half-ring providing a second line of points of contact.

7. A disengageable axial thrust bearing according to claim 1 , wherein the rolling elements are balls.

8. A disengageable axial thrust bearing according to claim 1 , wherein the stationary thrust member forms a portion of the casing.

9. A disengageable axial thrust bearing according to claim 1 , wherein the thrust bearing includes a clearance localized between the first pre-loading system between the outer half-ring and the casing, wherein said clearance is not zero so long as the axial load exerted on the axial thrust bearing is less than the determined threshold value.

10. The use of a disengageable axial thrust bearing according to claim 1 , in a cryogenic rotary machine, fitted with an active system for axial balancing under steady conditions.

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 2, 2015
From: BOUFFLERT, SÉBASTIEN; BOURDIN, PHILIPPE; LEMAITRE, ALBAN; TESSIER, FABIEN
To: SNECMA
Reel/Frame 036938/0847 →
Priority Claims (1)
FR 13 52806 · Mar 28, 2013 · national
Continuity (1)
Related Publication 20160032964A1 · Feb 4, 2016