Heat shrinkable film tube and method for manufacturing hollow composite parts

Patent metadata

Field	Value
Publication number	US-10293552-B2
Application number	US-201514943516-A
Country	US
Kind code	B2
Filing date	Nov 17, 2015
Priority date	Nov 17, 2015
Publication date	May 21, 2019
Grant date	May 21, 2019

Abstract

A film tube installed and sealed in a hollow composite part acts as an internal vacuum bag that eliminates the need for an internal mandrel to react compaction forces applied by autoclave pressure during curing of the part.

First claim

What is claimed is:

1. A method of processing a composite part, comprising:
placing a composite part on a tool having a tool cavity;
applying a film over an outer surface of a mandrel;
placing the mandrel inside a cavity in the composite part;
folding outer extremities of the film onto itself such that a portion of an inner film layer faces walls of the tool; and
attaching the film to walls of the tool within the tool cavity.

2. The method of claim 1 , wherein applying the film over the outer surface of the mandrel includes:
sleeving a film tube over the mandrel; and
shrinking the film onto the mandrel.

3. The method of claim 2 , wherein attaching the film to the walls of the cavity includes sealing opposite ends of the film tube to the tool.

4. The method of claim 2 , further comprising:
sealing a vacuum bag over the composite part; and
attaching opposite ends of the film tube to the vacuum bag.

5. The method of claim 1 , further comprising:
curing the composite part, including applying autoclave pressure to the film inside the cavity.

6. The method of claim 1 , wherein applying the film includes shrink wrapping a release film and an air impermeable barrier film onto the mandrel.

7. The method of claim 1 , further comprising removing the mandrel from the cavity in the composite part.

8. A method of applying a vacuum bag over a composite part, comprising:
placing the composite part on a tool having a tool cavity;
applying a film over an outer surface of a mandrel;
placing the mandrel inside a cavity in the composite part;
folding outer extremities of the film onto itself such that a portion of an inner film layer faces walls of the tool; and
attaching the film to walls of the tool cavity.

9. The method of claim 8 , further comprising removing the mandrel from the cavity in the composite part.

10. A method of bagging a composite part having a cavity therein, comprising:
applying a cavity vacuum bag over an outer surface of a mandrel
folding outer extremities of the cavity vacuum bag onto itself such that a portion of a barrier film layer faces walls of a tool;
applying the cavity vacuum bag over an inner surface of the cavity in the composite part;
applying an outer vacuum bag over the composite part;
sealing the cavity vacuum bag to the outer vacuum bag and to walls of the tool; and
sealing the outer vacuum bag to the tool.

11. A method of fabricating a composite part having a cavity therein, comprising:
placing a flexible inner bag around a mandrel;
shrink wrapping the inner bag onto an outer surface of the mandrel;
placing the composite part on a tool;
placing the mandrel in the cavity;
folding outer extremities of the inner bag onto itself such that a portion of a barrier film layer faces walls of the tool;
sealing the inner bag to the tool;
removing the mandrel from the cavity;
sealing an outer bag over the composite part;
sealing the inner bag to the outer bag; and
curing the composite part in an autoclave.

12. The method of claim 11 , wherein placing the flexible inner bag around the mandrel includes:
enveloping the mandrel with an air impermeable inner film; and
enveloping the inner film with an outer release film.

13. The method of claim 11 , wherein placing the flexible inner bag includes sleeving a film tube over the mandrel.

14. The method of claim 13 , wherein sealing the inner bag to the tool includes sealing outer ends of the film tube to the tool around substantially an entire circumference of the film tube.

15. The method of claim 11 , wherein shrink wrapping the inner bag includes applying heat to the flexible inner bag until the inner bag shrinks onto the outer surface of the mandrel.

16. The method of claim 11 , wherein sealing the inner bag to the outer bag includes:
adhering the portions of an inner face to the outer bag.

17. The method of claim 11 , wherein curing the composite part includes:
placing the composite part and the tool in an autoclave; and
exposing the outer bag and inner bag to autoclave pressure.

18. A method of fabricating a composite stringer having a cavity therein, comprising:
placing a composite stringer charge on a tool;
installing a flexible outer film bag over the composite stringer charge covering the cavity;
placing a flexible inner film bag in the cavity;
folding outer extremities of the inner film bag onto itself such that a portion of an inner film layer faces walls of the tool; and
compacting the composite stringer charge by applying pressure to the inner film bag and the outer film bag.

19. The method of claim 18 , wherein placing the inner film bag inside the cavity includes:
shrink wrapping an air impermeable barrier film tube around a mandrel;
placing the mandrel inside the cavity;
attaching the barrier film tube to the tool; and
removing the mandrel from the cavity.

20. The method of claim 18 wherein applying pressure to the inner film bag and the outer film bag is performed by placing the composite stringer charge and the tool in an autoclave, and subjecting the inner and outer film bags to autoclave pressure.

21. The method of claim 18 , wherein applying pressure is performed using a common pressure source.

22. The method of claim 21 , wherein applying pressure using a common pressure source includes:
placing the composite stringer charge in an autoclave; and
subjecting the inner film bag and the outer film bag to autoclave pressure.

Assignees

• Boeing Co

Inventors

• Heath Richard
• Modin Andrew Elmer

Classifications

• B29C70/446

  Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames · CPC title

• B29C47/0026

  Operations & Transport · mapped topic

• B29C66/81431

  comprising a single cavity, e.g. a groove · CPC title

• B29K2877/00

  Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as mould material · CPC title

• B29C35/02

  Heating or curing, e.g. crosslinking or vulcanizing {during moulding, e.g. in a mould}(cold vulcanisation B29C35/18 {; vulcanising tyres, presses therefor B29D30/0601}) · CPC title