IP Library Granted Patent US 7,244,098
Granted Patent B2
US 7,244,098 · App. 11/355,883 · Granted Jul 17, 2007

Device for adjusting the centering of a ring for synchronizing the control of pivoting vanes in a turbomachine

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Quick Facts
Patent No.
US 7,244,098
App. No.
11/355,883
Granted
Jul 17, 2007
Kind
B2
Abstract

The invention provides a device for adjusting the centering of a control ring for pivoting vanes of a turbomachine, the device comprising a plurality of pads for coming into contact with a circular surface that is coaxial with the ring, each pivoting vane being connected to the control ring via a lever having a first end secured to the control ring via a crank pin disposed radially on said ring, and a second end mounted on a pivot of the vane, each of said pads being secured to a pad carrier. Each pad carrier is secured under the control ring by means of attachment systems that are designed to be assembled from over the ring.

Claims (31)

1. A device for adjusting the centering of a control ring for pivoting vanes of a turbomachine, the device comprising a plurality of pads for coming into contact with a circular surface that is coaxial with the ring, each pivoting vane being connected to the control ring via a lever having a first end secured to the control ring via a crank pin disposed radially on said ring, and a second end mounted on a pivot of the vane, each of said pads being secured to a pad carrier, wherein each pad carrier is secured under the control ring by attachment systems that are designed to be assembled from over the rings,

wherein the pad carrier includes a substantially tubular portion extending longitudinally from the control ring towards the inside thereof and suitable for receiving a complementary tubular portion of the pad, the device further including a screw for screwing into the complementary tubular portion of the pad in such a manner as to enable the radial position of the pad to be adjusted.

2. A device according to claim 1 , further including means for adjusting the radial positions of the pads.

3. A device according to claim 1 , further including means for locking the pad against turning relative to the pad carrier.

4. A device according to claim 3 , wherein the respective tubular portions of the pad carrier and of the pad present respective right sections that are substantially polygonal so as to prevent the pad from turning in the pad carrier.

5. A device according to claim 1 , further including means for locking the adjustment screw in the pad.

6. A device according to claim 1 , wherein each pad carrier is disposed radially in line with the crank pin of the vane with which it is associated.

7. A device according to claim 1 , wherein each attachment system comprises a screw for screwing into the control ring from the outside thereof, and a clamping nut.

8. A stage of stator vanes of a compressor comprising at least one device according to claim 1 .

9. A turbomachine comprising at least one device according to claim 1 .

10. A device for mounting a pad on a control ring of a turbomachine, the device comprising:

a pad;

a pad carrier, wherein said pad is secured to said pad carrier;

a fastener configured to secure said pad carrier under the control ring, said fastener having a portion extending over said control ring when said pad carrier is secured under said control ring; and

a spring interposed between the pad carrier and the pad so as to provide damping for the pad.

11. A device for mounting a pad on a control ring of a turbomachine, the device comprising:

a pad;

a crank pin disposed radially on said control ring;

a pad carrier, wherein said pad is secured to said pad carrier;

a fastener configured to secure said pad carrier under the control ring, said fastener having a portion extending over said control ring when said pad carrier is secured under said control ring,

wherein the pad carrier is secured to the control ring with two attachment systems that are disposed symmetrically on either side of the crank pin.

12. A device for mounting a pad on a control ring of a turbomachine, the device comprising:

a pad;

a crank pin disposed radially on said control ring;

a pad carrier coupled to said pad, said pad carrier being positioned between said control ring and said pad, said pad carrier comprising two flanges disposed symmetrically on either side of the crank pin; and

two fasteners configured to secure said pad carrier to the control ring, each of said two fasteners extending through one of said two flanges of said pad carrier and through said control ring so that each of said two fasteners has a first free end on a side of said control ring and a second free end on another side of said control ring, said second free end being positioned between said control ring and said pad.

13. A device according to claim 12 , wherein said two fasteners are not coaxial with said pad carrier.

14. A device according to claim 12 , wherein said pad carrier is coaxial with said crank pin, and said fasteners are not coaxial with said pad carrier.

15. A device according to claim 12 , further comprising a spring interposed between the pad carrier and the pad.

16. A device according to claim 12 , further comprising a screw, and wherein said pad includes a hollow tubular portion, said screw extending from said control ring and into said hollow tubular portion of said pad.

17. A device according to claim 16 , wherein said screw has a head located between said control ring and said pad.

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 Feb 17, 2006
From: BROMANN, ALAIN, MARC, LUCIEN
To: SNECMA
Reel/Frame 017597/0339 →