IP Library Granted Patent US 9,926,944
Granted Patent B2
US 9,926,944 · App. 14/341,966 · Granted Mar 27, 2018

Device for guiding variable pitch diffuser vanes of a turbine engine

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 9,926,944
App. No.
14/341,966
Granted
Mar 27, 2018
Kind
B2
Abstract

A device for guiding variable pitch diffuser vanes of a turbine engine is provided. The device includes a first ring having an axial portion at its periphery that is extended by a collar extending radially outwards; a second ring mounted around the axial portion of the first ring so as to cooperate therewith to define a plurality of outwardly open sockets; a plurality of cylindrical bushings, each mounted in a respective socket for the purpose of receiving a guide pivot of a diffuser vane; and a resilient clamping ring for cooperating with one of the rings in order to clamp the two rings axially one against the other.

Claims (22)

1. A device for guiding variable pitch diffuser vanes of a turbine engine, the device comprising:

a first ring having an axial portion at a periphery of the first ring that is extended by a collar extending radially outwards;

a second ring mounted around the axial portion of the first ring so as to cooperate therewith to define a plurality of outwardly open sockets;

a plurality of cylindrical bushings, each mounted in a respective socket for the purpose of receiving a guide pivot of a diffuser vane; and

a resilient clamping ring carrying radial teeth, for cooperating with at least one of the first and second rings in order to clamp the first and second rings axially one against the other,

wherein the first ring or the second ring has a face with a profile that slopes radially, and the resilient clamping ring cooperates with said face,

wherein the first ring has a plurality of angular cutouts in the axial portion of the first ring in order to accommodate the radial teeth carried by the clamping ring, and

wherein the teeth of the clamping ring extend radially outwards and the second ring has a side face with a profile that slopes radially.

2. A device according to claim 1 , wherein the clamping ring is designed initially to be retracted in order to pass inside the first ring, and then to be released in order to enable the teeth to pass radially through the cutouts in the first ring and bear radially against the sloping side face of the second ring so as to exert an axial force clamping the two rings one against the other.

3. A device for guiding variable pitch diffuser vanes of a turbine engine, the device comprising:

a first ring having an axial portion at a periphery of the first ring that is extended by a collar extending radially outwards;

a second ring mounted around the axial portion of the first ring so as to cooperate therewith to define a plurality of outwardly open sockets;

a plurality of cylindrical bushings, each mounted in a respective socket for the purpose of receiving a guide pivot of a diffuser vane; and

a resilient clamping ring carrying radial teeth, for cooperating with at least one of the first and second rings in order to clamp the first and second rings axially one against the other,

wherein the first ring or the second ring has a face with a profile that slopes radially, and the resilient clamping ring cooperates with said face,

wherein the first ring has a plurality of angular cutouts in the axial portion of the first ring in order to accommodate the radial teeth carried by the clamping ring, and

wherein the teeth of the clamping ring extend radially inwards, the cutouts in the first ring each having a profile that slopes radially, and the second ring has an inwardly open annular groove.

4. A device according to claim 3 , wherein the clamping ring is designed initially to be opened up to be received completely within the groove in the second ring, and then to be released in order to enable the teeth to pass radially through the cutouts in the first ring and block the second ring axially in position so as to exert an axial force clamping the two rings one against the other.

5. A device according to claim 1 , wherein the clamping ring is an open ring or a spiral ring.

6. A device according to claim 1 , wherein the first ring and the second ring include indentations for receiving the bushings.

7. A device according to claim 3 , wherein the clamping ring is an open ring or a spiral ring.

8. A device according to claim 3 , wherein the first ring and the second ring include indentations for receiving the bushings.

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 Sep 5, 2014
From: MOUTON, CLEMENTINE CHARLOTTE MARIE; BELMONTE, OLIVIER; BROMANN, ALAIN MARC LUCIEN; LAO, JEREMY PHORLA
To: SNECMA
Reel/Frame 033676/0148 →