IP Library Granted Patent US 7,217,100
Granted Patent B2
US 7,217,100 · App. 10/893,259 · Granted May 15, 2007

Holding system for a rotor end plate

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Quick Facts
Patent No.
US 7,217,100
App. No.
10/893,259
Granted
May 15, 2007
Kind
B2
Abstract

A device for holding an annular end plate against a radial face of a rotor disc, the disc having in the radial face an annular recess behind a collar extending radially outwards, and the end plate having, in its radially inner part, an annular base bearing against the radially outer wall of the recess and a foot extending radially inwards in the recess from the base, the device including a split annular retaining ring disposed in the recess. The ring is constituted by a snap ring interposed axially between the foot of the end plate and the collar and the peripheral surface of which butts against the base, the peripheral surface and the collar comprising, when joined, notches, which open radially outwards and are intended to receive compression tools for the snap ring, which tools retract into the contour of the collar during the assembly or disassembly of the end plate.

Claims (27)

1. A device for holding an annular end plate against a radial face of a rotor disc, the disc having in the radial face an annular recess delimited by a plurality of walls, one of which is formed by an inside face of a collar extending radially outwards, and the end plate having, in its radially inner part, an annular base bearing against a radially outer wall of the recess and a foot extending radially inwards in the recess from the base, the device comprising:

a split annular retaining ring disposed in the recess, this ring having a first radial surface bearing against the inside face of the collar, a second radial surface bearing against an axially outside face of the foot and a peripheral surface butting against the foot or the base,

wherein the ring is a snap ring interposed axially between the foot of the end plate and the collar, and the peripheral surface of the ring butts against the base, the peripheral surface of the ring including a first plurality of notches and the collar including a corresponding second plurality of notches, both first and second plurality of notches open radially outwards and are configured to line up to receive compression tools for the snap ring, which tools retract into a contour of the collar during assembly or disassembly of the end plate.

2. The device according to claim 1 , wherein a radially inner portion of the snap ring is accommodated in a slot made behind the collar.

3. The device according to claim 2 , wherein the slot has a U-shaped section.

4. The device according to either of claims 2 or 3 , wherein a shoulder formed by the slot and a wall of the cavity has a diameter equal to or less than a diameter of the collar.

5. The device according to claim 4 , wherein the diameter of the shoulder is equal to or less than a diameter of a bottom of the notches in the collar.

6. The device according to claim 2 , wherein the snap ring has flat, opposing radial faces and a thickness of the snap ring is equal to or less than a width of the slot.

7. The device according to claim 1 , wherein the foot of the end plate has a bore, a diameter of which is substantially equal to a diameter of the collar.

8. A turbomachine including the device according to claim 1 .

9. A device comprising:

a disc having in a radial face an annular recess delimited by a plurality of walls, one of which is formed by an inside face of a collar extending radially outwards;

an end plate having in a radially inner part an annular base bearing against a radially outer wall of the recess and a foot extending radially inwards in the recess from the base;

a split annular retaining ring disposed in the recess, the ring having a first radial surface bearing against an inside face of the collar, a second radial surface bearing against an axially outside face of the foot, and a peripheral surface butting against the foot or the base, the ring being a snap ring interposed axially between the foot of the end plate and the collar, and the peripheral surface of the ring butting against the base, the peripheral surface of the ring including a first plurality of notches and the collar including a corresponding second plurality of notches, both first and second plurality of notches open radially outwards and are configured to line up to receive compression tools for the snap ring, which tools retract into the contour of the collar during assembly or disassembly of the end plate.

10. The device according to claim 9 , wherein a radially inner portion of the snap ring is accommodated in a slot made behind the collar.

11. The device according to claim 10 , wherein the slot has a U-shaped section.

12. The device according to claim 10 , wherein a shoulder formed by a slot and a wall of the cavity has a diameter equal to or less than a diameter of the collar.

13. The device according to claim 12 , wherein the diameter of the shoulder is equal to or less than a diameter of a bottom of the notches in the collar.

14. The device according to claim 10 , wherein the snap ring has flat, opposing radial faces and a thickness of the snap ring is equal to or less than a width of the slot.

15. The device according to claim 9 , wherein the foot of the end plate has a bore, a diameter of which is substantially equal to a diameter of the collar.

16. A turbomachine including the device according to claim 9 .

17. A device comprising:

a disc having in a radial face an annular recess delimited by a plurality of walls, one of which is formed by an inside face of a collar extending radially outwards;

an end plate having in a radially inner part an annular base bearing against a radially outer wall of the recess and a foot extending radially inwards in the recess from the base;

retaining means disposed in the recess, the retaining means having a first radial surface bearing against an inside face of the collar, a second radial surface bearing against an axially outside face of the foot, and a peripheral surface butting against the foot or the base, the retaining means being a snap retaining means interposed axially between the foot of the end plate and the collar, and the peripheral surface of the retaining means butting against the base, the peripheral surface of the retaining means including a first plurality of notches and the collar including a corresponding second plurality of notches, both first and second plurality of notches open radially outwards and are configured to line up to receive compression tools for the snap retaining means, which tools retract into the contour of the collar during assembly or disassembly of the end plate.

18. The device according to claim 17 , wherein the foot of the end plate has a bore, a diameter of which is substantially equal to a diameter of the collar.

19. A turbomachine including the device according to claim 17 .

Assignments (2)
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 →