Bearing with lubrication means and system for changing the pitch of the blades of a turboprop propeller of an aircraft equipped with said bearing

Patent metadata

Field	Value
Publication number	US-9951651-B2
Application number	US-201314405240-A
Country	US
Kind code	B2
Filing date	Jun 27, 2013
Priority date	Jun 27, 2012
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

A bearing, such as a rolling bearing, is mounted on a support mobile in translation and includes a lubrication mechanism. The lubrication mechanism includes at least one pipe delivering a lubricant, linked to a lubricant supply source, and at least partially engaging in the support mobile in translation to deliver the lubricant from the mobile support along an internal channel to the bearing, passing through an inner ring of the bearing.

First claim

The invention claimed is:

1. An assembly comprising:
a bearing including an inner ring;
a linear-movement actuator including
a cylindrical fixed part including a fixed piston, and
a movable external rod which is disposed around the cylindrical fixed part and which moves in translation by sliding about the fixed piston, the movable external rod including a lateral wall which delimits two opposing variable-volume chambers opposite each other, and the inner ring of the bearing being mounted around the movable external rod;

a pipe for conveying a lubricant from a lubricant supply source; and
a conduit connected to the movable external rod, in which engages, at least in part, the conduit having an internal path for conveying the lubricant from the movable external rod to the bearing, and passing the lubricant through the inner ring of the bearing,
wherein the pipe and the conduit extend parallel to the translational movement of the movable external rod to cooperate with each other by sliding between first and second positions of the moveable external rod, the pipe being fixed and the conduit sliding with respect thereto.

2. The assembly according to claim 1 , wherein the conduit is provided in a lateral wall of the movable external rod, and wherein the internal path comprises at least one hole made in the inner ring of the bearing and in communication with the conduit.

3. The assembly according to claim 2 , wherein the pipe comprises a plurality of pipes distributed angularly with respect to one another and communicating, on an upstream side, with a common element comprising a common conduit, for conveying the lubricant, connected to the lubricant supply source, and wherein said conduit comprises a plurality of conduits, and said pipes engaging, on a downstream side, in respective conduits provided in correspondence in a wall of the movable external rod.

4. The assembly according to claim 1 , wherein the movable external rod and the cylindrical fixed part of the linear-movement actuator are interconnected in rotation by a connection tube supported by transverse end faces of the movable external rod and associated with the cylindrical fixed part, the connection tube including an internal passage forming the conduit configured to receive the pipe conveying the lubricant.

5. The assembly according to claim 4 , wherein the internal passage comprises first and second portions, the first portion for conveying the lubricant through the internal passage in the movable external rod of the linear-movement actuator, and the second portion for conveying the lubricant from the internal passage to the bearing.

6. The assembly according to claim 5 , wherein the second portion is defined by orifices formed in correspondence in the connection tube and a relevant transverse face of the movable external rod, and by an annular chamber formed between the lateral wall of the movable external rod and a sleeve for annular support of the inner ring of the bearing, and communicating with the orifices and the inner ring of the bearing.

7. A system for changing a pitch of vanes of a turboshaft engine propeller having a longitudinal axis for an aircraft, comprising:
an assembly according to claim 1 ; and
a connection mechanism for transforming translation of the movable external rod of the linear-movement actuator into a rotation of the vanes to modify a pitch thereof, and a means of transmission between the outer ring of the bearing and the vanes.

8. A turbine engine comprising:
coaxial and contrarotatory propulsion propellers, upstream and downstream respectively,
wherein at least the upstream propeller comprises a system for changing the pitch of the vanes according to claim 7 .

Assignees

• Snecma

Inventors

• Frantz Caroline
• Igel Dominik
• Hugon Nadege
• Curlier Augustin

Classifications

• F16C33/6677 Primary

  from radial inside, e.g. via a passage through the shaft and/or inner ring · CPC title

• F16C23/06

  Ball or roller bearings · CPC title

• F01D7/00

  Rotors with blades adjustable in operation; Control thereof (for reversing F01D1/30) · CPC title

• B64D2027/005

  Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR] · CPC title

• B64C11/306

  specially adapted for contrarotating propellers · CPC title