Method for producing a compressor stator of an axial turbomachine

Patent metadata

Field	Value
Publication number	US-10436220-B2
Application number	US-201515326618-A
Country	US
Kind code	B2
Filing date	Jul 13, 2015
Priority date	Jul 31, 2014
Publication date	Oct 8, 2019
Grant date	Oct 8, 2019

Abstract

The invention relates to a method of producing a low-pressure compressor stator for an axial turbine engine. The stator comprises an external shroud with stubs and an annular row of stator blades extending radially towards the inside from the stubs. The method comprises the following stages: supply or production of a starting bar; bending of the bar so that it makes a circle, in order to form an unwrought external shroud; turning to form an axial annular wall delimited by annular fixing flanges; orbital friction-welding of a row of blades onto the stubs of the external shroud. The stubs are realized during a milling stage of the bar or of the external shroud, the milling being carried out before or after the bending stage. The shroud and the blades can be produced in titanium or in a thermoplastic polymer.

First claim

The invention claimed is:

1. A method of producing an axial turbine engine stator, the stator comprising an external shroud with an internal surface and an annular row of stator blades extending radially towards the inside from the external shroud, the method comprising the following stages, performed in that order:
a) supplying a material bar;
b) bending of the bar so that it makes a circle, in order to form an external shroud; and
c) welding a row of blades onto the external shroud, wherein the internal surface of the external shroud comprises blade-receiving portions that are generally perpendicular to the radial direction and are formed on blade stubs; and during the welding stage (c), the blades are friction-welded onto the blade-receiving portions.

2. The method according to claim 1 , wherein during the welding stage (c), the blades are orbital friction-welded.

3. The method according to claim 2 , wherein after the bending stage (b), the method comprises at least one turning stage of the external shroud.

4. The method according to claim 3 , wherein the turning stage comprises the production of an external annular groove extending axially to the right of the welds of the blades on the shroud and an internal tubular support intended to receive an annular seal and formed at a distance axially from the welds.

5. The method according to claim 4 , wherein the turning stage comprises the formation of an annular bead that extends radially towards the outside and that is disposed axially to the right of the welds of the blades on the shroud.

6. The method according to claim 5 further comprising a milling stage of the bar, so as to form the blade stubs on the bar, the milling stage being realized before the bending stage.

7. The method according to claim 6 , wherein the external shroud comprises a generally annular wall with a rotational profile extending mainly axially, a radial height of the blade stubs being at least two times greater than a thickness of the annular wall.

8. The method according to claim 7 , wherein during the welding stage (c) at least one or every blade of the annular row of stator blades is/are welded while being rubbed against a respective receiving portion of the blade-receiving portions according to a movement comprising a component along the chord of the blade.

9. The method according to claim 8 , wherein the blade-receiving portions form an annular row of planar surfaces or a generally tubular or truncated annular surface.

10. The method according to claim 9 , wherein the external shroud comprises a generally annular wall with a rotational profile extending mainly axially and at least one, annular fixing flange extending radially towards the outside, each annular flange being disposed at one axial end of the annular wall.

11. The method according to claim 7 , wherein the radial height of the blade stubs is at least three times greater than a thickness of the annular wall.

12. The method according to claim 5 further comprising a milling stage of the shroud, so as to form blade stubs on the external shroud, the milling stage being realized after the bending stage (b) and the blade-receiving portions being formed on the stubs.

13. The method according to claim 12 , wherein the milling stage is realized after the turning stage.

14. The method according to claim 1 , wherein:
the external shroud and the blades are made of a metallic material; or
the external shroud and the blades are produced from thermoplastic polymer materials.

15. The method according to claim 14 , wherein the external shroud and the blades are made of titanium.

16. A method of producing a turbine engine comprising a plurality of stators, each stator comprising an external shroud associated with a row of blades and be fixed axially to one another, said method of producing the turbine engine comprising a method of producing the stator, wherein the method of producing stator comprising the following stages, performed in that order:
a) supplying a material bar;
b) bending of the bar so that it makes a circle, in order to form an external shroud; and
c) welding a row of blades onto the external shroud, wherein the internal surface of the shroud comprises blade-receiving portions that are generally perpendicular to the radial direction and are formed on blade stubs; and during the welding stage (c), the blades are friction-welded onto the blade-receiving portions.

Assignees

• Safran Aero Boosters Sa
• Safran Aero Boosters Sa

Inventors

• Hindryckx Francois

Classifications

• B29C66/73921

  characterised by the materials of both parts being thermoplastics · CPC title

• B23K20/233

  without ferrous layer · CPC title

• B23K20/26

  Auxiliary equipment · CPC title

• B29C53/36

  Bending and joining, e.g. for making hollow articles (B29C53/56 takes precedence) · CPC title

• B23K20/12

  the heat being generated by friction; Friction welding · CPC title