Blade-retaining plate with internal cut-outs for a turbomachine stator

Patent metadata

Field	Value
Publication number	US-9771815-B2
Application number	US-201314136070-A
Country	US
Kind code	B2
Filing date	Dec 20, 2013
Priority date	Dec 24, 2012
Publication date	Sep 26, 2017
Grant date	Sep 26, 2017

Abstract

The invention relates to an axial turbomachine stator ( 2 ) comprising an inner shell ( 28 ) with an annular row of openings; an annular row of blades ( 26 ); the said blades extending substantially radially through the said openings, respectively, and each comprising a cut-out ( 34 ) on the inside of the shell; at least one blade-retaining plate ( 36 ) inserted in at least one cut-out ( 34 ), with means of immobilization of the said plate in the cut-out(s). The means of immobilization comprise at least one tongue ( 38 ) with an end forming a support surface ( 40 ) in contact with a part of the blade ( 26 ) or of one of the blades ( 26 ) located radially directly above the corresponding cut-out.

First claim

The invention claimed is:

1. Axial turbomachine stator, comprising:
an internal shell with an annular row of openings;
an annular row of blades, the blades extending substantially radially through the openings, respectively, and each blade comprising a closed cut-out on an inner side of the shell; and
at least one blade-retaining flat plate inserted into at least one of the cut-outs, with means of immobilization of the plate in the at least one of the cut-outs;
wherein the means of immobilization comprise at least one tongue angled relative to the flat plate and with an end forming a support surface in contact with a part of the blade with the corresponding cut-out, said part being located radially in alignment with the corresponding cut-out and distinct from said cut-out;
wherein the plate passes through the cut-outs of at least two adjacent blades.

2. Stator in accordance with claim 1 , wherein the part of each blade in contact with the support surface of the at least one tongue is located between the cut-out and the internal shell.

3. Stator in accordance with claim 1 , wherein the support surface extends along the blade substantially parallel to a mean plane of the plate.

4. Stator in accordance with claim 1 , wherein the at least one tongue is designed to deform essentially along a predominantly axial deformation axis.

5. Stator in accordance with claim 1 , wherein the at least one tongue is elastically deformable so as to take its support position after insertion of the plate in the at least one of the cut-outs.

6. Stator in accordance with claim 1 , wherein the at least one tongue is plastically deformable so as to enable its insertion from a position essentially within the extent the plate.

7. Stator in accordance with claim 1 , wherein the at least one tongue is integral with the plate and cut out from the said plate in the general shape of a U.

8. Stator in accordance with claim 1 , wherein the at least one tongue has edges that lie within the outline of the plate.

9. Stator in accordance with claim 1 , wherein the plate comprises two tongues pointing in opposite directions.

10. Stator in accordance with claim 9 , wherein the two tongues cooperate respectively with faces of each of the at least two adjacent blades, the faces facing each other.

11. Stator in accordance with claim 9 , wherein the two tongues cooperate respectively with faces of each of the at least two adjacent blades, the faces being opposite one another.

12. Stator in accordance with claim 1 , further comprising:
at least two tongues pointing in opposite directions, the two tongues cooperating, each and respectively, with a face of the blade or one of the blades.

13. Stator in accordance with claim 1 , wherein the plate has an end configured to abut against one face of the blade or one of the blades, the tongue being in contact with an opposite face of the blade or with a corresponding face of another blade.

14. Stator in accordance with claim 1 , wherein the support surface of the at least one tongue contacts the blade with the corresponding cut-out via an elastomeric material applied to the blade at the corresponding opening in the shell, the elastomeric material retaining the blade in the shell and/or providing a seal between the blade and the shell.

15. A turbomachine, comprising:
an internal shell with an annular row of openings;
an annular row of blades, the blades extending substantially radially through the openings, respectively, and each blade comprising a closed cut-out on an inner side of the shell; and
at least one blade-retaining flat plate inserted into at least one of the cut-outs, with means of immobilization of the plate in the at least one of the cut-outs;
wherein the means of immobilization comprise at least one tongue angled relative to the flat plate and with an end forming a support surface in contact with a part of the blade of the corresponding cut-out, said part being located radially next to the corresponding cut-out and distinct from said cut-out;
wherein the plate passes through the cut-outs of at least two adjacent blades.

Assignees

• Techspace Aero Sa
• Safran Aero Boosters Sa

Inventors

• Remy Christophe

Classifications

• F01D9/042 Primary

  fixing blades to stators (fixing stator-rings in the casing or to each other F01D25/246) · CPC title

• F01D25/246

  Fastening of diaphragms or stator-rings · CPC title

• F04D29/54

  Fluid-guiding means, e.g. diffusers · CPC title

• F01D9/04 Primary

  forming ring or sector · CPC title