IP Library Granted Patent US 10,113,824
Granted Patent B2
US 10,113,824 · App. 15/650,262 · Granted Oct 30, 2018

Composite projectile barrel

Inventors: Peter Darcy Kowalski (Morrinsville, NZ); Stephen Robert Mitchell McGuire (Rotoorangi, NZ)
Assignee: K & M INNOVATIONS LIMITED
F41A21/02B32B5/022B32B5/024B32B5/26B32B7/005B32B1/08B32B2250/05B32B2250/20B32B2305/076B32B2305/188B32B2305/20B32B2331/00B32B2363/00B32B2597/00
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Quick Facts
Patent No.
US 10,113,824
App. No.
15/650,262
Granted
Oct 30, 2018
Kind
B2
Abstract

A composite projectile barrel having an inner barrel section and a composite outer barrel shell aligned coaxially with the inner barrel section is described. The inner barrel section may be made from a metal or metal alloy. The composite outer barrel shell may include two or more layers of carbon fiber prepreg and a layer of non-woven nanofiber web membrane disposed between adjacent layer of carbon fiber prepreg. The carbon fiber prepreg can include a weave of carbon fibers in a nanoparticle-reinforced resin matrix, with the resin content being less than or equal to 35 wt % of the carbon fiber content. The non-woven nanofiber web membrane can be Xantu.layr™.

Claims (27)

1. A composite projectile barrel comprising:

an inner barrel section having a bore extending through the length of the inner barrel section; and

a composite outer barrel section coaxially aligned with the inner barrel section, the composite outer barrel section comprising:

at least two layers of a carbon fiber prepreg; and

at least one layer of a non-woven nanofiber web membrane disposed between adjacent layers of carbon fiber prepreg;

wherein the interior surface of the composite outer barrel section is in direct contact with the exterior surface of the inner barrel section.

2. The composite projectile barrel of claim 1 , wherein the carbon fiber prepreg comprises a weave of carbon fibers in a nanoparticle-reinforced resin matrix.

3. The composite projectile barrel of claim 2 , wherein the nanoparticle-reinforced resin matrix content is less than or equal to 35 wt % of the carbon fiber content.

4. The composite projectile barrel of claim 2 , wherein the nanoparticle-reinforced resin matrix comprises a resin having a glass transition temperature of 220° C. or greater.

5. The composite projectile barrel of claim 1 , wherein the at least one layer of non-woven nanofiber web membrane comprises Xantu.layr™.

6. The composite projectile barrel of claim 1 , wherein the inner barrel section comprises a metal alloy.

7. The composite projectile barrel of claim 6 , wherein the metal alloy is a steel alloy.

8. The composite projectile barrel of claim 2 , wherein the resin of the nanoparticle-reinforced resin matrix is an epoxy resin.

9. The composite projectile barrel of claim 2 , wherein the resin of the nanoparticle-reinforced resin matrix is a phenolic resin.

10. The composite projectile barrel of claim 2 , wherein the resin of the nanoparticle-reinforced resin matrix is a polyester resin.

11. The composite projectile barrel of claim 1 , wherein the inner barrel section comprises an intermediate tapered portion.

12. The composite projectile barrel of claim 1 , wherein the inner barrel section comprises an intermediate recess into which the composite outer barrel section is disposed.

13. The composite projectile barrel of claim 1 , wherein the composite outer barrel section comprises:

four to six inner layers of unidirectional carbon fiber prepreg oriented in a direction parallel to the direction of the bore;

two to four intermediate layers of unidirectional carbon fiber prepreg oriented at a 45° angle to the direction of the bore;

one to three outer layers of unidirectional carbon fiber prepreg oriented at a 90° angle to the direction of the bore; and

a layer of a non-woven nanofiber web membrane disposed between each adjacent layers of carbon fiber prepreg.

14. The composite projectile barrel of claim 13 , wherein the composite outer barrel section comprises:

five inner layers of unidirectional carbon fiber prepreg oriented in a direction parallel to the direction of the bore;

three intermediate layers of unidirectional carbon fiber prepreg oriented at a 45° angle to the direction of the bore;

two outer layers of unidirectional carbon fiber prepreg oriented at a 90° angle to the direction of the bore; and

a layer of a non-woven nanofiber web membrane disposed between each adjacent layers of carbon fiber prepreg.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 29, 2022
From: K & M INNOVATIONS LIMITED
To: MCGUIRE, STEPHEN ROBERT MITCHELL
Reel/Frame 060218/0149 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 22, 2018
From: KOWALSKI, PETER DARCY; MCGUIRE, STEPHEN ROBERT MITCHELL
To: K & M INNOVATIONS LIMITED
Reel/Frame 044693/0094 →
Continuity (2)
Provisional Application 62362260 · Jul 14, 2016
Related Publication 20180017350A1 · Jan 18, 2018