# US 5,348,598 A · Method of manufacturing a gun barrel provided with a lining

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- Number: US 5,348,598 A
- Document ID: US5348598A
- Status: Granted
- Kind: A
- Application number: 07/892,179
- Filed: 1992-06-02
- Granted: 1994-09-20
- Earliest claimed: 1991-06-06
- Assignees: Societe Europeenne de Propulsion
- Inventors: Michel Vives; Pierre Taveau; Georges Habarou; Francois Bognandi
- Web page: https://patentgrep.com/patent/US5348598A

## CPC

- F41A 21/02: Composite barrels, i.e. barrels having multiple layers, e.g. of different materials
- F41A: FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE

## Abstract

A gun barrel lining made of composite material having refractory fiber reinforcement and a ceramic matrix, the fiber reinforcement comprises a cylindrical inner portion constituted by a three-dimensional fiber texture and a cylindrical outer portion surrounding the inner portion and having the same axis, the outer portion being constituted by a strip wound around the inner portion, and the inner and outer portions being codensified by the ceramic matrix.

## Claims

### Claim 1

A method of manufacturing a gun barrel lining in a composite material by forming a cylindrical fibrous reinforcement and densifying the reinforcement by a ceramic matrix, said method comprising the steps of:
providing a first fibrous texture;
winding said first fibrous texture in superposed layers and binding said superposed layers by causing fibers to extend transversely through said superposed layers, to form a cylindrical and three-dimensional inner portion of said reinforcement;
providing a second fibrous texture made of refractory fibers;
winding said second fibrous texture onto said inner portion of said reinforcement, to form a cylindrical outer portion of said reinforcement;
said inner portion of said reinforcement is made by winding and bonding together layers of fibers of a precursor of refractory fibers and the precursor is transformed into refractory fibers by heat treatment prior to winding of the second texture; and
simultaneously densifying said inner portion of said reinforcement and said outer portion of said reinforcement with a ceramic matrix.

### Claim 2 (depends on 1)

The method of claim 1, wherein said inner portion of said reinforcement includes carbon fibers.

### Claim 3 (depends on 1)

The method of claim 1, wherein said first fibrous texture includes fibers of a carbon precursor.

### Claim 4 (depends on 3)

The method of claim 3, wherein said first fibrous texture includes polyacrylonitrile.

### Claim 5 (depends on 1)

The method of claim 1, wherein said second fibrous texture includes ceramic fibers.

### Claim 6 (depends on 1)

The method of claim 1, wherein said binding includes needling.

### Claim 7 (depends on 1)

The method of claim 1, wherein said binding includes implanting threads through said layers.

### Claim 8 (depends on 1)

The method of claim 1, wherein said inner portion of said reinforcement is formed by winding superposed layers of said first fibrous texture and needling said layers together along directions that mutually intersect.

### Claim 9 (depends on 1)

The method of claim 1, wherein said inner portion of said reinforcement and said outer portion of said reinforcement are codensified by chemical vapor infiltration.

### Claim 10 (depends on 1)

The method of claim 1, wherein said inner portion of said reinforcement and said outer portion of said reinforcement are codensified by means of a liquid.