IP Library Granted Patent US 8,732,977
Granted Patent B2
US 8,732,977 · App. 11/776,929 · Granted May 27, 2014

Method of producing structural components having improved toughness

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Quick Facts
Patent No.
US 8,732,977
App. No.
11/776,929
Granted
May 27, 2014
Kind
B2
Abstract

A method of producing a structural component comprising manufacturing a structural component from a moisture absorbable material the toughness of which increases with increasing moisture absorption and subsequently subjecting the structural component to at least one of elevated temperature and humidity for a period of time such that the structural component attains a predetermined moisture content and distribution.

Claims (32)

1. A method of producing a structural component from a moisture absorbing material, comprising:

determining a moisture content and a distribution of the moisture absorbing material according to a desired increase in toughness of the moisture absorbing material;

manufacturing the structural component from two or more plies of the moisture absorbable material, the toughness of which increases with increasing moisture absorption; and subsequently

conditioning, in a conditioning chamber, the structural component to at least one of elevated temperature and humidity for a period of time sufficient to introduce a known and predetermined level of moisture to one or more outer plies of the structural component whereby the structural component attains the predetermined moisture content and distribution, wherein the predetermined moisture distribution comprises an inner portion of the structural component that is moisture free and an outer portion extending from the inner portion to a surface of the structural component, the outer portion having a moisture content that increases from a minimum adjacent to the inner portion to a maximum at the surface of the structural component; and

when the predetermined moisture content and distribution is attained the structural component is removed from the conditioning chamber.

2. The method of claim 1 , wherein the desired increase in toughness is determined by stress calculations.

3. The method of claim 1 , wherein the desired increase in toughness is determined by experimentation.

4. The method of claim 1 , wherein the duration of the period of time over which the structural component is conditioned to at least one of the elevated temperature and humidity is previously determined by numerical modeling of the moisture diffusion of the material.

5. The method of claim 1 , wherein the period of time over which the structural component is conditioned to at least one of the elevated temperature and humidity is previously determined by numerical modeling of the moisture diffusion of the material and is determined by periodically weighing the structural component to determine the moisture content, the time period ending when the predetermined moisture content is reached.

6. The method of claim 1 , wherein the moisture absorbable material comprises a composite material.

7. The method of claim 1 , wherein the structural component comprises an aircraft component.

8. The method of claim 1 , wherein the predetermined moisture content and distribution is limited to 2-4 mm of the outer material of the structural component.

9. The method of claim 1 , wherein the predetermined moisture content and distribution is limited to 10-11 mm of the outer material of the structural component.

10. The method of claim 1 , wherein the structural component is conditioned at 70 degrees C. and 85% relative humidity.

11. The method of claim 1 , wherein the structural component is conditioned at the elevated temperature and humidity for at least six weeks.

12. The method of claim 1 , wherein the structural component is a finished structural component.

13. A method of producing a structural component from a moisture absorbing material comprising a composite material which comprises epoxy resin matrix carbon fibre, comprising:

determining a moisture content and a distribution of the moisture absorbing material according to a desired increase in toughness of the moisture absorbing material;

manufacturing the structural component from two or more plies of the moisture absorbable material, the toughness of which increases with increasing moisture absorption; and subsequently

conditioning, in a conditioning chamber, the structural component to at least one of elevated temperature and humidity for a period of time sufficient to introduce a known and predetermined level of moisture to one or more outer plies of the structural component whereby the structural component attains the predetermined moisture content and distribution, wherein the predetermined moisture distribution comprises an inner portion of the structural component that is moisture free and an outer portion extending from the inner portion to a surface of the structural component, the outer portion having a moisture content that increases from a minimum adjacent to the inner portion to a maximum at the surface of the structural component; and

when the predetermined moisture content and distribution is attained the structural component is removed from the conditioning chamber.

14. The method of claim 13 , wherein the structural component is conditioned at 70 degrees C. and 85% relative humidity.

15. The method of claim 13 , wherein the outer portion is limited to 2-4 mm.

16. The method of claim 13 , wherein the finished structural component is conditioned at elevated temperature and humidity for at least six weeks.

17. The method of claim 13 , wherein the structural component is a finished structural component.

18. The method of claim 13 , wherein the structural component comprises an aircraft component.

19. A method of producing a structural component from a moisture absorbing material, comprising:

determining a moisture content and a distribution of the moisture absorbing material according to a desired increase in toughness of the moisture absorbing material;

manufacturing a non-composite plastic structural component from two or more plies of the moisture absorbable material, the toughness of which increases with increasing moisture absorption, and subsequently

conditioning, in a conditioning chamber, the non-composite plastic structural component to at least one of elevated temperature and humidity for a period of time sufficient to introduce a known and predetermined level of moisture to one or more outer plies of the structural component whereby the structural component attains the predetermined moisture content and distribution, wherein the predetermined moisture distribution comprises an inner portion of the structural component that is moisture free and an outer portion extending from the inner portion to a surface of the structural component, the outer portion having a moisture content that increases from a minimum adjacent to the inner portion to a maximum at the surface of the structural component; and

when the predetermined moisture content and distribution is attained the structural component is removed from the conditioning chamber.

20. The method of claim 19 , wherein the structural component is conditioned at 70 degrees C. and 85% relative humidity.

Assignments (2)
CHANGE OF NAME Recorded Apr 18, 2011
From: AIRBUS UK LIMITED
To: AIRBUS OPERATIONS LIMITED
Reel/Frame 026141/0311 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 12, 2007
From: ADAMS, RICHARD; GRIGGS, PETER; WATSON, GLENN
To: AIRBUS UK LIMITED
Reel/Frame 019551/0134 →