Mould for an abradable track beneath the inner shroud of an axial-flow turbomachine compressor

Patent metadata

Field	Value
Publication number	US-10132180-B2
Application number	US-201514728362-A
Country	US
Kind code	B2
Filing date	Jun 2, 2015
Priority date	Jun 5, 2014
Publication date	Nov 20, 2018
Grant date	Nov 20, 2018

Abstract

The invention relates to a mold for injecting a layer of abradable material, such as silicone, inside an inner shroud of an axial-flow turbomachine. The mold comprises a circular wall or tubular wall extending axially and two annular walls extending radially outwardly from the axial ends of the axial wall. Each radial wall of the mold comprises an annular hook in contact with the outer surface of the shroud so as to hold the mold against the shroud. The injection pressure presses the hooks against the shroud, providing a seal. The walls form an annular molding cavity inside the inner shroud in combination with the inner shroud. The invention also relates to a method for molding an abradable layer inside the shroud with the aid of the mold. The latter is deformed by spreading apart the hooks so as to fit over the shroud.

First claim

What is claimed is:

1. A kit including a shroud of an axial-flow turbomachine and a mold for injecting a layer of abradable material inside the shroud, the shroud comprising an annular outer surface radially opposed to the abradable layer, said mold comprising:
a circular axial wall extending axially and including:
a first circular axial end; and
a second axial end; and

two annular walls extending radially outwardly from one of the first axial end and the second axial end of the circular axial wall, the walls of the mold structured and operable to form an annular molding cavity inside the shroud in combination with the shroud,
wherein each radial wall of the mold comprises an annular hook structured and operable to be in circular contact with the annular outer surface of the shroud so as to allow the mold to be radially held in relation to the shroud's annular outer surface, and
wherein the radially outer ends of the radial walls have outer conical guide surfaces, which spread apart from one another outwardly so as to facilitate the spreading of the hooks as the shroud is inserted into the mold.

2. The kit of claim 1 , wherein the hooks form annular grooves that are open axially towards one another, each hook comprises an annular retention surface structured and operable to allow a radial retention between the hook and the shroud, and an annular stop surface structured and operable to come into radial abutment against the shroud, the annular surfaces being coaxial.

3. The kit of claim 1 , wherein the mold is segmented, at least one of the segments comprises planar and parallel ends, along the circumference, and at least one of the segments comprises planar ends of which the planes are inclined by at least 60°.

4. The mould kit of claim 3 , wherein the mold is formed from two to sixteen angular segments, and it is made of a polymeric material.

5. The kit of claim 1 , wherein the axial wall comprises a thinner annular portion disposed axially at the center thereof.

6. The kit of claim 1 , wherein the minimum thickness of the axial wall is less than the average thickness of the radial walls.

7. The kit of claim 1 , wherein the axial length of the axial wall is greater than the radial height of each radial wall.

8. A method for molding a resin layer of abradable material inside the shroud of an axial-flow turbomachine, said method comprising the steps of:
providing a shroud of a turbomachine;
providing a mold with two annular hooks configured to hold the mold against the shroud, wherein the mold comprises:
a circular axial wall extending axially and including:
a first circular axial end,
and a second axial end;

two annular walls extending radially outwardly from one of the first axial end and the second axial end of the circular axial wall;
the walls of the mold structured and operable to form an annular molding cavity inside the shroud in combination with the shroud,
wherein each radial wall of the mold comprises a respective one of the annular hooks structured and operable to be in circular contact with the annular outer surface of the shroud so as to allow the mold to be radially held in relation to the shroud's annular outer surface,
wherein the radially outer ends of the radial walls have outer conical guide surfaces, which spread apart from one another outwardly so as to facilitate the spreading of the hooks as the shroud is inserted into the mold;

placing the mold against the shroud, the shroud being engaged in the hooks by distancing the hooks from one another, so as to define an annular molding cavity inside the shroud; and
injecting a resin inside the molding cavity in order to form a layer of abradable material inside the shroud.

9. The method of claim 8 , wherein each hook forms a seal between the mold and the shroud.

10. The method of claim 9 , wherein the hooks comprise a smooth annular surface forming a circular seal between the mold and the shroud.

11. The method of claim 8 , wherein placing the mold against the shroud comprises pressing the mold radially against the shroud in an outer direction.

12. The method of claim 8 , wherein the hooks each have at least a radial stop surface and at least a radial retention surface for retaining the mold on the shroud, the surfaces being radially opposed and possibly annular, and in that, during placing the mold against the shroud, each radial stop surface hugs the shroud over the entire length thereof.

13. The method of claim 8 , wherein the mold comprises an annular wall extending axially between the hooks, and in that, during placing the mold against the shroud, the axial wall is bent.

14. The method of claim 13 , wherein during injection, the resin exerts a pressure against the axial wall and arches the axial wall so as to bring the annular hooks closer together, and to press the annular hooks against the shroud, and the resin comprises silicone.

Assignees

• Techspace Aero Sa
• Safran Aero Boosters Sa

Inventors

• Leszczynski Charles
• Biemar Guy

Classifications

• F05D2230/90

  Coating; Surface treatment · CPC title

• F04D29/164

  of an axial flow wheel · CPC title

• F05D2220/30

  in turbines · CPC title

• F05D2230/31

  Layer deposition · CPC title

• B29C70/74

  Moulding material on a relatively small portion of the preformed part, e.g. outsert moulding {(B29C70/845 takes precedence)} · CPC title