IP Library Granted Patent US 7,510,332
Granted Patent B2
US 7,510,332 · App. 11/283,818 · Granted Mar 31, 2009

Compensation for an insufficient supply of lubricant in an inter-shaft bearing

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Quick Facts
Patent No.
US 7,510,332
App. No.
11/283,818
Granted
Mar 31, 2009
Kind
B2
Abstract

The quality of the lubrication of an inter-shaft bearing, particularly one with counter-rotational bushes, is improved by the presence of an obstacle on the outer bush which allows an adjustment in the quantity of oil present on the outer roll track. In particular, the drying of the roll track under the effect of the repeated running of the runners is compensated for by organizing a mandatory axial circulation.

Claims (28)

1. A rolling bearing including:

an outer bush having an inner surface delimiting a generally cylindrical cavity and including a first roll track;

an inner bush having a generally cylindrical outer surface including a second roll track;

a roller unit placed between the first and second roll tracks and having an outer surface of a shape complementary to the first roll track;

wherein each of the rollers, outer bush and inner bush is mounted to rotate freely around its axis of rotation;

wherein the outer bush includes a protuberance located on its inner surface laterally relative to the first roll track and the protuberance is configured to guide an axial circulation of flow of lubricant through a clearance between the outer surface of the roller unit and a diameter of the first roll track.

2. The rolling bearing according to claim 1 wherein the protuberance is located at a distance from the first roll track lower than or equal to half the width of the outer surface of the rollers.

3. The rolling bearing according to claim 2 wherein the protuberance is formed unitarily with the outer bush.

4. The rolling bearing according to claim 3 additionally including a trough clearance adjacent to the protuberance on the side of the first roll track.

5. The rolling bearing according to claim 3 wherein the inner bush includes at least one lubricant fluid inlet.

6. The rolling bearing according to claim 2 wherein the protuberance is in the form of a continuous projection along the periphery of a cavity over the inner surface.

7. The rolling bearing according to claim 6 wherein the protuberance comprises an elastic washer located in a continuous groove along the periphery of a cavity on inner surface.

8. The rolling bearing according to claim 7 wherein the inner bush includes at least one lubricant fluid inlet.

9. The rolling bearing according to claim 1 including a slot located on the inner surface of the outer bush at a distance from the first roll track less than or equal to half the width of the outer surface of the rollers.

10. The rolling bearing according to claim 9 wherein the slot is in the form of a continuous groove along the periphery of the cavity on inner surface.

11. The rolling bearing according to claim 10 additionally including an elastic washer configured to be located in the groove and to be held therein.

12. A turbine engine comprising a rolling bearing according to claim 1 .

13. The rolling bearing according to claim 1 wherein the inner bush includes at least one lubricant fluid inlet.

14. The roller bearing according to claim 13 , wherein the at least one fluid inlet is disposed, in an axial direction, closer to the protuberance than is a portion of the roller unit farthest from the protuberance.

15. The roller bearing according claim 14 , wherein a fluid channel extends along the inner surface of the outer bush and away from the roller unit in an axial direction on a side of the roller unit opposite a side on which the protuberance is disposed, and the fluid channel includes a first portion with a first thickness, as measured in a radial direction, and a second portion disposed farther from the protuberance, as measured in the axial direction, than the first portion, the second portion having a second thickness in the radial direction smaller than the first thickness.

16. A shaft assembly of an engine comprising:

a rolling bearing including an outer bush and an inner bush, one of the bushes being fastened to a shaft, and a roller unit configured to rotate freely between the two bushes, wherein the outer bush comprises a projecting part located on its inner surface and offset laterally relative to the roller unit,

wherein the inner bush includes at least one lubricant fluid inlet, and the projecting part is configured to guide lubricant fluid from the fluid inlet in an axial direction through a clearance between an outer surface of the roller unit and the outer bush.

17. The shaft assembly according to claim 16 wherein the projecting part is a projection of the outer bush.

18. The shaft assembly according to claim 16 wherein the projection is continuous around the inner surface.

19. The shaft assembly according to claim 16 wherein the projecting part is formed by a washer located in a groove disposed in the inner surface of the outer bush.

20. A turbine engine comprising the shaft assembly according to claim 16 .

21. The shaft according to claim 16 , wherein the outer surface of the roller unit facing the clearance is substantially parallel to the axial direction in which the lubricant fluid flows.

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 22, 2005
From: PLONA, DANIEL GEORGES
To: SNECMA
Reel/Frame 017273/0183 →