Shaping equipment and facility for gas-phase chemical infiltration of fibrous preforms

Patent metadata

Field	Value
Publication number	US-10906205-B2
Application number	US-201716467299-A
Country	US
Kind code	B2
Filing date	Dec 4, 2017
Priority date	Dec 7, 2016
Publication date	Feb 2, 2021
Grant date	Feb 2, 2021

Abstract

A shaping tooling for chemical vapor infiltration of a fiber preform includes a structural enclosure formed by supports each provided with a multiply-perforated zone. Each of the supports has in its inside face an uncased zone that includes the multiply-perforated zone. The shaping tooling further includes first and second shaping mold functional elements, each present in a respective one of the uncased zones of the support. Each shaping mold functional element has a first face of a determined shape corresponding to the shape of the part that is to be made and a second face that is held facing the inside face of a support. Each functional element has a plurality of perforations and presents a number of perforations, a size of perforations, or a shape of perforations that differs from the number, the size, or the shape of the perforations present in the facing support.

First claim

The invention claimed is:

1. Shaping tooling for chemical infiltration of a fiber preform, the tooling comprising a structural enclosure formed by at least a first support having a first multiply-perforated zone and a second support having a second multiply-perforated zone, the first and second supports being held one against the other,
wherein the first support includes on its inside face a first uncased zone including the first multiply-perforated zone, wherein the first multiply-perforated zone includes first perforations that extend entirely through the first support from an outside face of the first support to the inside face of the first support, wherein the second support includes in its inside face a second uncased zone including the second multiply perforated zone, wherein the second multiply-perforated zone includes second perforations that extend entirely through the second support from an outside face of the second support to the inside face of the second support, and wherein the shaping tooling further comprises at least first and second shaping mold functional elements present respectively in the first and second uncased zones of the first and second supports, each shaping mold functional element having a first face of a determined shape corresponding to a shape of the part that is to be made, and a second face held facing the inside face of one of the first and second supports, each shaping mold functional element having a plurality of perforations and presenting at least a number of perforations, a size of perforations, or a shape of perforations that differs from the number, the size, or the shape of the perforations present in said one of the first and second supports,
wherein the first multiply-perforated zone of the first uncased zone is surrounded by a first rim on which said first shaping mold rests such that said first multiply-perforated zone is spaced apart from the second face of said first shaping mold.

2. The tooling according to claim 1 , wherein a porous depletion layer is interposed between the inside face of each support of the structural enclosure and the second face of the shaping mold functional element held facing the inside face of said one of the first and second supports.

3. The tooling according to claim 2 , wherein the porous depletion layer is selected from one of the following textures: a carbon mat, a two-dimensional carbon fabric, a carbon felt.

4. The tooling according to claim 1 , wherein the first and second supports and the first and second shaping mold functional elements are made of a material selected from at least one of the following materials: graphite, carbon/carbon composite material, and ceramic matrix composite material.

5. A charge for placing in an installation for densification by chemical vapor infiltration, said charge comprising a fiber preform held in shaping tooling according to claim 1 .

6. The charge according to claim 5 , wherein the fiber preform is a preform for an aeroengine part.

7. An assembly comprising an installation for densification of a fiber preform by chemical vapor infiltration, the assembly comprising a reaction chamber, a reagent gas feed pipe situated at a first end of the chamber and leading into a preheating zone, and a discharge pipe situated in the vicinity of a second end, the assembly also including at least one charge according to claim 5 situated in the chamber.

8. A method of fabricating a composite material part, the method comprising:
placing a fiber preform in shaping tooling according to claim 1 ;
consolidating the fiber preform with a matrix by chemical vapor infiltration; and
densifying the consolidated preform.

9. The tooling according to claim 1 , wherein the second multiply-perforated zone of the second uncased zone is surrounded by a second rim on which said second shaping mold rests such that said second multiply-perforated zone is spaced apart from the second face of said second shaping mold.

Assignees

• Safran Ceram

Inventors

• Thibaud Simon
• Delcamp Adrien
• BERTRAND SéBASTIEN
• GOUJARD STéPHANE

Classifications

• C23C16/45563

  Gas nozzles · CPC title

• C23C16/455

  characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber · CPC title

• C23C16/4582

  Rigid and flat substrates, e.g. plates or discs (C23C16/4581 takes precedence) · CPC title

• C04B41/4584

  Coating or impregnating of particulate or fibrous ceramic material (C04B20/10, C04B35/628 take precedence) · CPC title

• C04B41/4531

  by C.V.D. · CPC title