Method for producing a double-walled thermostructural monolithic composite part, and part produced

Patent metadata

Field	Value
Publication number	US-10759713-B2
Application number	US-201515514900-A
Country	US
Kind code	B2
Filing date	Sep 24, 2015
Priority date	Oct 2, 2014
Publication date	Sep 1, 2020
Grant date	Sep 1, 2020

Abstract

A fibrous preform ( 1 ) is produced, provided with a sandwich structure comprising an intermediate flexible core ( 4 ) and two outer fibrous frames ( 2, 3 ), respectively arranged on opposing outer faces of said flexible core ( 4 ) and assembled by sections of wire ( 8, 9 ) passing through said fibrous frames ( 2, 3 ), said preform ( 1 ) being impregnated with resin. Said preform is then hardened and the core ( 4 ) is removed, preferably by pre-densification with chemical vapour infiltration, and the structure produced is then densified with liquid-phase infiltration.

First claim

The invention claimed is:

1. A method for producing a thermostructural monolithic fibres/matrix composite part, comprising two skins of composite material which are spaced apart from one another and interconnected by a plurality of thread-like spacers of composite material, said method comprising at least:
A/ producing a fibrous preform provided with a sandwich structure comprising an intermediate flexible core and two outer fibrous frames arranged on opposed outer faces of said flexible core and joined by thread portions that pass through said fibrous frames, said preform being impregnated with resin;
B/ curing said preform and removing said core; and
C/ densifying a resulting structure,
wherein, in step B/, pre-densification is carried out by gas-phase infiltration so as to pre-densify said preform and thus said thread portions intended for forming said spacers, said gas-phase infiltration providing said thread portions with a layer that protects said thread portions during step C/, and said core being removed by the pre-densification by gas-phase infiltration,
wherein, in step C/, said structure is densified by liquid-phase infiltration.

2. The method according to claim 1 , wherein, in an intermediate step between steps B/ and C/, the preform that was pre-densified in step B/ is machined.

3. The method according to claim 1 , wherein, in step C/, in order to achieve liquid-phase densification, silicon is introduced in liquid paste form and spreads out under heat and pressure in a densification furnace.

4. The method according to claim 1 , wherein, in step A/, a fibrous preform having variable thickness is produced.

5. The method according to claim 1 , wherein, in step A/:
a) said sandwich structure is a flexible sandwich structure that comprises said intermediate flexible core, which is made of a material that is capable of being penetrated by a needle and is impervious to the resin, and said two outer fibrous frames that are flexible fibrous frames arranged on and opposed outer faces of said flexible core;
b) said fibrous frames and said core of said sandwich structure are joined by stitching by means of a thread forming stitches that include said thread portions that pass through said fibrous frames and said core, said thread consisting of a roving comprising a plurality of filaments that are not linked together, said thread portions that pass through said fibrous frames and said core having, following said stitching operation, longitudinal channels in said core that are provided between said filaments and extend from one of said fibrous frames to the other; and
c) said sandwich structure is impregnated with said resin, said impregnation operation being carried out such that said resin is made to penetrate said longitudinal channels of said thread portions in order to form, at the location of each of said portions, a resin bridge, of which opposed ends are in contact with the resin impregnating said flexible fibrous frames.

6. The method according to claim 1 , wherein said layer that protects said thread portions during step C/ is a carbon layer.

7. A method for producing a thermostructural monolithic fibres/matrix composite part, comprising two skins of composite material which are spaced apart from one another and interconnected by a plurality of thread-like spacers of composite material, said method comprising at least:
A/ producing a fibrous preform provided with a sandwich structure comprising an intermediate flexible core and two outer fibrous frames arranged on opposed outer faces of said flexible core and joined by thread portions that pass through said fibrous frames, said preform being impregnated with resin;
B/ curing said preform and removing said core; and
C/ densifying the resulting structure,
wherein, in step C/, said structure is densified by liquid-phase infiltration,
wherein, in step B/, pre-densification is carried out by gas-phase infiltration so as to pre-densify said preform and thus said thread portions intended for forming said spacers,
wherein, in an intermediate step between steps B/ and C/, the preform that was pre-densified in step B/ is machined, and
wherein, in said intermediate step, threaded holes and/or bores are machined.

8. The method according to claim 7 , wherein, at least during the densification step, step C/, plugs are arranged in said threaded holes and/or said bores.

Assignees

• Mbda France
• Airbus Defence & Space Gmbh

Inventors

• Bouchez Marc
• Beyer Steffen
• Schmidt-Wimmer Stephan

Classifications

• C04B35/65

  Reaction sintering of free metal- or free silicon-containing compositions {(C04B35/573, C04B35/591 take precedence)} · CPC title

• C04B35/62878

  with boron or silicon · CPC title

• C04B35/62873

  Carbon · CPC title

• C04B35/573 Primary

  obtained by reaction sintering {or recrystallisation} · CPC title

• B29C70/68 Primary

  by incorporating or moulding on preformed parts, e.g. inserts or layers {, e.g. foam blocks (mould constructions therefor B29C33/12; joining preformed parts by moulding B29C65/70)} · CPC title