IP Library Granted Patent US 9,222,363
Granted Patent B2
US 9,222,363 · App. 13/805,142 · Granted Dec 29, 2015

Angular sector of a stator for a turbine engine compressor, a turbine engine stator, and a turbine engine including such a sector

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Quick Facts
Patent No.
US 9,222,363
App. No.
13/805,142
Granted
Dec 29, 2015
Kind
B2
Abstract

A stator angular sector for a turbine engine compressor and including: an outer shroud and an inner shroud; and at least one vane extending radially between the shrouds and connected thereto at its radial ends. At one of its axial ends the outer shroud includes a cavity opening out to the axial end and extending between a radially-inner tongue of the outer shroud to which the radially-outer end of the vane is connected and a radially-outer tongue of the outer shroud carrying a mounting mechanism for mounting the stator angular sector to a casing of the engine. An abutment-forming insert is housed at least in part in the cavity, the abutment-forming insert configured to limit radial movements of the radially-inner tongue by contact and thus to modify vibratory behavior of the radially-inner tongue.

Claims (20)

1. A stator angular sector for a turbine engine compressor, the sector extending around an axis of radial symmetry and comprising:

an outer shroud and an inner shroud arranged coaxially one inside the other; and

at least one vane extending radially between the shrouds and connected thereto at its radial ends;

wherein the outer shroud includes mounting means at each of its axial ends for mounting the stator angular sector to a casing of the engine;

wherein the outer shroud includes, at least one axial end, a cavity opening out to the axial end, the cavity extending between a radially-inner tongue of the outer shroud to which the radially-outer end of the vane is connected and a radially-outer tongue of the outer shroud carrying the mounting means for mounting the stator angular sector to the casing of the engine; and

wherein at least one abutment-forming insert is housed at least in part in the cavity, the abutment-forming insert configured to limit radial movements of the radially-inner tongue by contact and thus to modify vibratory behavior of the radially-inner tongue.

2. A stator angular sector according to claim 1 , wherein the outer shroud includes an upstream cavity opening out to an upstream end of the outer shroud and a downstream cavity opening out to a downstream end of the outer shroud, at least one abutment-forming insert being housed in at least one of the cavities.

3. A stator angular sector according to claim 1 , wherein the outer shroud is made as a single piece.

4. A stator angular sector according to claim 1 , wherein clearance exists between the abutment-forming insert and the radially-inner tongue and/or between the abutment-forming insert and the radially-outer tongue of the outer shroud.

5. A stator angular sector according to claim 1 , wherein the abutment-forming insert is in effortless contact with the radially-inner tongue and/or the radially-outer tongue of the outer shroud.

6. A stator angular sector according to claim 1 , wherein the abutment-forming insert is clamped radially against the radially-inner tongue and/or the radially-outer tongue of the outer shroud.

7. A stator angular sector according to claim 1 , wherein at least one of the radial ends of the abutment-forming insert co-operates with an annular groove portion of complementary shape provided in the outer shroud, whereby the insert is held in position in the axial direction.

8. A stator angular sector according to claim 1 , wherein a radial end of the abutment-forming insert is fastened to the outer shroud by a brazed connection.

9. A stator angular sector according to claim 8 , wherein the brazed connection connects the abutment-forming insert to the radially-outer tongue of the outer shroud.

10. A stator angular sector according to claim 1 , wherein the abutment-forming insert is a ring portion having an oblong shape in an axial plane, and the radially-inner and outer ends of the ring portion co-operate with respective annular groove portions formed in the radially-inner tongue and in the radially-outer tongue.

11. A stator angular sector according to claim 1 , wherein the abutment-forming insert is a ring portion having one of its radial ends co-operating with an annular groove portion of complementary shape provided in the outer shroud, and its other radial end connected to the outer shroud by a brazed connection.

12. A stator angular sector according to claim 1 , wherein the abutment-forming insert is a ring portion having a base forming a portion of a cylinder situated facing the radially-inner tongue, and a middle portion extending radially outwards from the base to the radially-outer tongue of the outer shroud.

13. A stator angular sector according to claim 12 , wherein the base forming a portion of a cylinder includes at least one indentation in its radially-inner face.

14. A turbine engine stator comprising one or more stator angular sectors according to claim 1 .

15. A turbine engine including at least one stator according to claim 14 .

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 Apr 3, 2013
From: CLOAREC, YVON
To: SNECMA
Reel/Frame 030141/0179 →