Method for producing a part consisting of a composite material

Patent metadata

Field	Value
Publication number	US-11097345-B2
Application number	US-201615750008-A
Country	US
Kind code	B2
Filing date	Aug 2, 2016
Priority date	Aug 6, 2015
Publication date	Aug 24, 2021
Grant date	Aug 24, 2021

Abstract

A method includes fabricating a part out of composite material including fiber reinforcement densified by a metal matrix.

First claim

The invention claimed is:

1. A method of fabricating a part out of composite material comprising fiber reinforcement densified by a metal matrix, the method comprising at least the following steps:
a) positioning a plurality of fibers comprising a core each made of ceramic material coated by a metal sheath on a first preform for a first portion of the part to be fabricated, said first preform comprising at least a metal powder of a first alloy and a first binder, wherein the first preform is present on a support and between two side walls of the support, the fibers being present on the first preform and on the side walls and positioning elements being positioned on each of the side walls, each of the positioning elements presenting a plurality of teeth between which the fibers are received, thereby serving to hold the fibers stationary relative to the positioning elements in a desired orientation;
b) positioning a second preform for a second portion of the part to be fabricated on the first preform in order to obtain a stack structure, the fibers being present between the first preform and the second preform in said stack structure, said second preform comprising at least a metal powder of a second alloy and a second binder, the melting temperature T 1 of the first alloy, the melting temperature T 2 of the second alloy, and the melting temperature T 3 of the metal sheaths of the fibers satisfying the following two conditions:
| T 3 −T 1 |/T 1 ≤25%, and

| T 3 −T 2 |/T 2 ≤25%,

melting temperatures T 1 , T 2 and T 3 being expressed in degrees Celsius;
c) eliminating the first and second binders present in the stack structure obtained after performing step b) in order to obtain a debindered stack structure, the stack structure being removed from the support and the fibers being removed from gaps between the teeth before eliminating the first and second binders; and
d) heat treating the debindered stack structure in order to obtain the part during which the metal sheaths of the fibers are assembled with the powders of the first and second alloys by diffusion welding and during which the metal powder of the first alloy and the metal powder of the second alloy are sintered in order to form the metal matrix.

2. A method according to claim 1 , wherein the following two conditions are satisfied:
| T 3 −T 1 |/T 1 ≤15% and

| T 3 −T 2 |/T 2 ≤15%.

3. A method according to claim 1 , wherein the first and second preforms are each formed by performing a metal injection molding method.

4. A method according to claim 1 , wherein the metal sheaths of the fibers, the first alloy, and the second alloy are each constituted in the majority by weight by a same metal element.

5. A method according to claim 1 , wherein the material forming the metal sheaths of the fibers is identical to the first alloy and/or the second alloy.

6. A method according to claim 1 , wherein the fibers are received, in the stack structure, in grooves formed in the surface of the first preform and/or in the surface of the second preform.

7. A method according to claim 1 , wherein the metal sheaths of all or some of the fibers are in the form of continuous layers of a metal material.

8. A method according to claim 1 , wherein the metal sheaths of all or some of the fibers are in the form of respective pluralities of metal strands surrounding the cores.

9. A method according to claim 1 , wherein the fibers comprise a first set of fibers extending along a first direction and a second set of fibers extending along a second direction that is not parallel to the first direction.

10. A method according to claim 1 , wherein the first alloy is identical to the second alloy.

11. A method according to claim 1 , wherein the first alloy and the second alloy are selected from: titanium-based alloys, nickel-based alloys, cobalt-based alloys, aluminum-based alloys, and steels.

12. A method of fabricating a part out of composite material comprising fiber reinforcement densified by a metal matrix, the method comprising at least the following steps:
a) positioning a plurality of fibers comprising a core each made of ceramic material coated by a metal sheath on a first preform for a first portion of the part to be fabricated, said first preform comprising at least a metal powder of a first alloy and a first binder; wherein the first preform is present on a support and between two side walls of the support, the fibers being present on the first preform and on the side walls and positioning elements being positioned on each of the side walls, each of the positioning elements presenting at least one opening positioned in register with an associated opening in the side walls, and each of the positioning elements presenting a plurality of teeth between which the fibers are received, thereby serving to hold the fibers stationary relative to the positioning elements in a desired orientation;
b) positioning a second preform for a second portion of the part to be fabricated on the first preform in order to obtain a stack structure, the fibers being present between the first preform and the second preform in said stack structure, said second preform comprising at least a metal powder of a second alloy and a second binder, the melting temperature T 1 of the first alloy, the melting temperature T 2 of the second alloy, and the melting temperature T 3 of the metal sheaths of the fibers satisfying the following two conditions:
| T 3 −T 1 |/T 1 ≤25%, and

| T 3 −T 2 |/T 2 ≤25%,

the melting temperatures T 1 , T 2 and T 3 being expressed in degrees Celsius;
c) eliminating the first and second binders present in the stack structure obtained after performing step b) in order to obtain a debindered stack structure; and
d) heat treating the debindered stack structure in order to obtain the composite material part during which the metal sheaths of the fibers are assembled with the powders of the first and second alloys by diffusion welding and during which the powders of the first and second alloys are sintered in order to form the metal matrix.

13. A method according to claim 12 , wherein the following conditions are satisfied:
| T 3 −T 1 |/T 1 ≤15% and

| T 3 −T 2 |/T 2 ≤15%.

14. A method according to claim 12 , wherein the first and second preforms are each formed by performing a metal injection molding method.

15. A method according to claim 12 , wherein the metal sheaths of the fibers, the first alloy, and the second alloy are each constituted in the majority by weight by a same metal element.

16. A method according to claim 12 , wherein the material forming the metal sheaths of the fibers is identical to the first alloy and/or the second alloy.

17. A method according to claim 12 , wherein the fibers are received, in the stack structure, in grooves formed in the surface of the first preform and/or in the surface of the second preform.

18. A method according to claim 12 , wherein the metal sheaths of all or some of the fibers are in the form of continuous layers of a metal material.

19. A method according to claim 12 , wherein the fibers comprise a first set of fibers extending along a first direction and a second set of fibers extending along a second direction that is not parallel to the first direction.

20. A method according to claim 12 , wherein the first alloy is identical to the second alloy.

Assignees

• Safran Aircraft Engines

Inventors

• Fribourg Guillaume

Classifications

• C22C47/025

  Aligning or orienting the fibres · CPC title

• C22C47/14

  by powder metallurgy, i.e. by processing mixtures of metal powder and fibres or filaments · CPC title

• B22F3/225

  by injection molding · CPC title

• B22F7/062 Primary

  involving the connection or repairing of preformed parts · CPC title

• C22C47/04

  by coating, e.g. with a protective or activated covering · CPC title