Assembly for an epicyclic reduction gearset comprising at least one satellite bearing comprising lubrication means

Patent metadata

Field	Value
Publication number	US-10697498-B2
Application number	US-201716074039-A
Country	US
Kind code	B2
Filing date	Jan 20, 2017
Priority date	Feb 1, 2016
Publication date	Jun 30, 2020
Grant date	Jun 30, 2020

Abstract

An assembly for an epicyclic reduction gearset, including a satellite carrier, satellites, and at least one satellite bearing including a central axis linked to the satellite carrier. An inner ring mounted on the central axis, an outer ring mounted to rotate around the central axis. A lubrication circuit brings a flow of oil between the rings. The lubrication circuit includes a first portion supplied with oil with openings to the outside of the inner ring in a radially inner area of the bearing. A second portion has openings to the outside of the inner ring. An intermediate portion has at least one channeling connecting the first portion to the second portion, having at least one singular pressure reduction formed by an elbow and at least one flattening of a transverse cross-section. The central axis has a radially outer first surface. The inner ring has a radially inner second surface.

First claim

The invention claimed is:

1. Assembly for an epicyclic reduction gearset, the assembly comprising a satellite carrier, satellites and at least one satellite bearing carried by the satellite carrier that is rotatable about an axis of rotation (X), said bearing comprising a central axis, an inner ring securely mounted on the central axis, an outer ring mounted to rotate around said central axis, and a lubrication circuit arranged to bring a flow of oil between said inner and outer rings, said lubrication circuit comprising a first portion arranged to be supplied with oil from the satellite carrier at the central axis and comprising openings opening to the outside of the inner ring in a radially inner area (B) of the bearing with respect to said axis of rotation (X), a second portion comprising openings opening to the outside of the inner ring in a radially outer area (A) of the bearing with respect to said axis of rotation (X), and an intermediate portion comprising at least one channeling arranged to connect the first portion to the second portion, said at least one channeling comprising at least one singular pressure drop formed by an elbow or a sudden narrowing of a cross-section and at least one flattening of a transverse cross-section over a major portion of the length thereof or a path forming a detour, wherein the central axis is linked to the satellite carrier and comprising a radially outer first surface with respect to said central axis, and the inner ring comprising a radially inner second surface with respect to said central axis, said first and second surfaces being joined, said at least one channeling being formed by a groove applied in the first or the second surface.

2. Assembly according to claim 1 , wherein the first and second surfaces are cylindrical and plain.

3. Assembly according to claim 1 , wherein the flattening of the transverse cross-section of said at least one channeling is obtained by applying in the first or the second surface, the groove corresponding substantially to an arc of a circle of which the radius of curvature is greater than half of the distance separating the edges of the groove on said first or second surface.

4. Assembly according to claim 1 , wherein at least one of the first and second portions of the lubrication circuit comprises said at least one channeling formed by the groove applied in the first or the second surface, communicating with at least one duct passing through the inner ring.

5. Assembly according to claim 4 , wherein the first portion of the lubrication circuit comprises said duct which extends substantially along a longitudinal axis, formed in said central axis and arranged to be supplied with lubricant at a first of its longitudinal ends, and wherein said at least one channeling formed by the groove applied in the first or the second surface, communicating with said duct by at least one outlet opening of the central axis.

6. Assembly according to claim 5 , wherein the first portion of the lubrication circuit comprises at least two grooves in the first or the second surface, in planes that are substantially perpendicular to the axis of rotation (X), each communicating with one opening of said openings passing through the inner ring.

7. Assembly according claim 6 , wherein said at least one channeling of the intermediate portion of the lubrication circuit is connected to at least one of said two grooves of the first portion of the lubrication circuit.

8. Assembly according to claim 7 , wherein said at least one channeling comprising a channeling in the intermediate portion of the lubrication circuit, said single channeling is connected to that of said at least two grooves of the first portion of the lubrication circuit which is the farthest away from said first longitudinal end of the longitudinal duct of the central axis.

Assignees

• Safran Trans Systems

Inventors

• Feraud Benjamin
• Benykhlef Aissa
• Gedin Patrice
• Beck Guillaume Julien

Classifications

• F16C2361/61

  Toothed gear systems, e.g. support of pinion shafts · CPC title

• F16C19/38

  with two or more rows of rollers · CPC title

• F16C33/586

  outside the space between the races, e.g. end faces or bore of inner ring · CPC title

• F16C23/086

  forming a track for rolling elements · CPC title

• F16H57/0482

  Gearings with gears having orbital motion · CPC title