IP Library Granted Patent US 7,347,672
Granted Patent B2
US 7,347,672 · App. 11/046,680 · Granted Mar 25, 2008

Rotor disk balancing device, disk fitted with such a device and rotor with such a disk

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Quick Facts
Patent No.
US 7,347,672
App. No.
11/046,680
Granted
Mar 25, 2008
Kind
B2
Abstract

A rotor disc includes a rim and a balancing device, which includes housings formed in the rim, and balancing masses housed in at least some of the housings.

Claims (57)

1. A rotor disk comprising:

a rim;

a plurality of blades integral with said rim;

housings formed in said rim, said housings defining orifices that open up on a same side face of the rim;

balancing masses housed in a first plurality of said housings; and

a spring retaining ring positioned laterally against the rim so as to only partially close off the orifices of the housings,

wherein a second plurality of said housings is free of said balancing masses.

2. A rotor disk according to claim 1 , wherein the housings are located under a platform that supports the plurality of blades.

3. A rotor disk according to claim 1 , wherein the housings are distributed around the circumference of the rim.

4. A rotor disk according to claim 1 , wherein the housings partially pass through the rim.

5. A rotor disk according to claim 1 , further comprising a circumferential slit into which the spring retaining ring is fitted.

6. A rotor disk according to claim 1 , wherein the spring retaining ring forms a protrusion designed to be fitted into one of the housings, to prevent the spring retaining ring from rotating axially.

7. A rotor disk according to claim 1 , wherein the housings pass through the rim between a first side face and a second side face of the rim opposite said first face.

8. A rotor disk according to claim 1 , wherein the shape of the housings and the balancing masses is adapted to prevent a rotation or tipping of the balancing masses in their corresponding housings.

9. A rotor disk according to claim 1 , wherein said housings in said first and second pluralities of housings have a same shape.

10. A rotor disk according to claim 9 , wherein said housings in said first and second pluralities of housings have a same size.

11. A rotor disk according to claim 10 , wherein said housings in said first and second pluralities of housings are circumferentially distributed around said rim and radially positioned between said blades and a connection flange configured to connect said rotor disk to another adjacent rotor disk.

12. A rotor disk according to claim 10 , wherein said first plurality of said housings that house said balancing masses and said second plurality of said housings that are free of said balancing masses are distributed around said rim such that said rotor disk is balanced.

13. A rotor disk according to claim 1 , wherein said housings in said second plurality of housings that are free of said balancing masses have a shape and a size configured to receive said balancing masses.

14. A rotor disk comprising:

a rim;

a plurality of blades integral with said rim;

housings formed in said rim; and

balancing masses housed in a first plurality of said housings,

wherein a second plurality of said housings is free of said balancing masses, the housings pass through the rim between a first side face and a second side face of the rim opposite said first face, the housings comprise a first cavity defining an orifice that opens up on the first side face of the rim, a second cavity defining an orifice that opens up on the second face of the rim, and wherein said housings define an intermediate channel connecting the first and second cavities.

15. A rotor disk according to claim 14 , wherein the balancing masses in said first plurality of housings are placed in the first cavities.

16. A rotor disk according to claim 15 , further comprising balancing masses placed in the intermediate channels of said first plurality of housings.

17. A rotor disk according to claim 14 , further comprising sealing flanges placed in the second cavities.

18. A rotor disk according to claim 14 , further comprising a first spring retaining ring, designed to be positioned laterally against the rim, so as to at least partially close off the orifices of the first cavities and a second spring retaining ring designed to be positioned laterally against the rim, so as to close off the orifices of the second cavities.

19. A rotor disk according to claim 18 , wherein the first spring retaining ring forms a protrusion fitted into one of the first cavities, to prevent the first spring retaining ring from rotating axially, and wherein the second spring retaining ring forms a protrusion fitted into one of the second cavities, to prevent the second spring retaining ring from rotating axially.

20. A rotor disk according to claim 18 , further comprising a first circumferential slit into which the first spring retaining ring is fitted, and a second circumferential slit into which the second spring retaining ring is fitted.

21. A rotor disk according to claim 18 , wherein each spring retaining ring closes off at least half of the orifices.

22. A rotor disk according to claim 21 , wherein each spring retaining ring completely closes off the orifices.

23. A rotor disk according to claim 18 , wherein each spring retaining ring closes off at least half of the orifices.

24. A rotor disk according to claim 23 , wherein each spring retaining ring completely closes off the orifices.

25. A rotor disk according to claim 14 , wherein the shape of the housings and the balancing masses is adapted to prevent a rotation or tipping of the balancing masses in their corresponding housings.

26. A rotor disk according to claim 14 , wherein said housings in said first and second pluralities of housings have a same shape.

27. A rotor disk according to claim 26 , wherein said housings in said first and second pluralities of housings have a same size.

28. A rotor disk according to claim 27 , wherein said housings in said first and second pluralities of housings are circumferentially distributed around said rim and radially positioned between said blades and a connection flange configured to connect said rotor disk to another adjacent rotor disk.

29. A rotor disk according to claim 27 , wherein said first plurality of said housings that house said balancing masses and said second plurality of said housings that are free of said balancing masses are distributed around said rim such that said rotor disk is balanced.

30. A rotor disk according to claim 14 , wherein said housings in said second plurality of housings that are free of said balancing masses have a shape and a size configured to receive said balancing masses.

31. A rotor comprising:

at least one disk, said disk comprising

a rim;

a plurality of blades integral with said rim;

housings formed in said rim, said housings defining orifices that open up on a same side face of the rim;

balancing masses housed in a first plurality of said housings; and

a spring retaining ring positioned laterally against the rim so as to only partially close off the orifices of the housings,

wherein a second plurality of said housings are free of said balancing masses.

32. A turbomachine comprising:

at least one rotor having at least one disk, said disk comprising

a rim;

a plurality of blades integral with said rim;

housings formed in said rim, said housings defining orifices that open up on a same side face of the rim;

balancing masses housed in a first plurality of said housings; and

a spring retaining ring positioned laterally against the rim so as to only partially close off the orifices of the housings,

wherein a second plurality of said housings are free of said balancing masses.

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 →