System and method for facilitating fluid movement in close-molded composite parts

Patent metadata

Field	Value
Publication number	US-9199419-B2
Application number	US-201213665721-A
Country	US
Kind code	B2
Filing date	Oct 31, 2012
Priority date	Oct 31, 2012
Publication date	Dec 1, 2015
Grant date	Dec 1, 2015

Abstract

A vacuum bagging system may include a layer assembly defining a fluid flow channel. The layer assembly may include a contact layer mounted to a composite part positionable within an outer mold line (OML) tool. The contact layer may have a contact layer width defined by opposing contact layer side edges. The layer assembly may further include an inner layer mounted to the contact layer and having inner layer side edges located between the contact layer side edges. The fluid flow channel may extend along at least a portion of the composite part to at least one part end. The vacuum bagging system may include an internal vacuum bag positionable against the inner layer. An inner mold line (IML) tool may support the internal vacuum bag. The contact layer width may be less than an IML tool width.

First claim

What is claimed is:

1. A method of forming a fluid flow channel in a vacuum bagging system, comprising the steps of:
mounting a strip of contact layer along a first portion of a part inner surface of a composite part formed of pre-impregnated fiber-reinforced material and positionable within an outer mold line tool, the strip of contact layer extending from a part interior of the composite part to at least one part end of the composite part and having a contact layer width defined by opposing contact layer side edges, the strip of contact layer being located adjacent to and outside of a second portion of the composite part such that an internal vacuum bag applies vacuum pressure directly onto the part inner surface of the second portion not covered by the strip of contact layer;
mounting a strip of inner layer to the strip of contact layer, the strip of inner layer having an inner layer width that is no greater than the contact layer width and being positioned between opposing contact layer side edges;
extending the contact layer to at least one part end of the composite part; and
positioning an internal vacuum bag on an interior of the part inner surface such that the internal vacuum bag is located on a side of the inner layer opposite the contact layer, the internal vacuum bag covering an inner mold line tool having an inner mold line tool width, the contact layer width of the strip of contact layer being less than the inner mold line tool width.

2. The method of claim 1 further comprising the step of:
drawing a vacuum on a tool interior between the part inner surface and the internal vacuum bag; and
drawing fluid along the fluid flow channel in response to drawing the vacuum on the tool interior.

3. The method of claim 2 wherein the step of drawing the vacuum on the tool interior comprises:
sealing an external vacuum bag over a tool end of the outer mold line tool.

4. The method of claim 1 further comprising the step of:
compacting the composite part positioned between an outer mold line tool surface and the internal vacuum bag in response to drawing the vacuum.

5. The method of claim 1 further comprising the step of:
removably securing the contact layer to the part inner surface of the composite part at one or more discrete locations.

6. The method of claim 1 further comprising the step of:
providing the contact layer in a contact layer width of no greater than approximately 3 inches.

7. The method of claim 1 further comprising the step of:
providing the contact layer at a contact layer thickness of no greater than approximately 0.005 inch.

8. The method of claim 1 further comprising the step of:
providing the inner layer at an inner layer thickness of no greater than approximately 0.050 inch.

9. The method of claim 1 further comprising the step of:
providing the contact layer, the inner layer, and the internal vacuum bag such that a total layer assembly thickness is no greater than approximately 0.10 inch.

10. The method of claim 1 further comprising the step of:
providing the internal vacuum bag as an assembly of at least two layers including a part-side bag layer and a non-part side layer, the part-side bag layer being in contact with the inner layer, the non-part side layer being in contact with the inner mold line tool.

11. The method of claim 1 wherein the step of positioning an internal vacuum bag on a side of the inner layer comprises:
drawing a vacuum on an interior of the internal vacuum bag;
installing the internal vacuum bag and the inner mold line tool within the composite part while drawing the vacuum on the interior of the internal vacuum bag; and
halting the vacuum applied to the interior of the internal vacuum bag.

Assignees

• Boeing Co

Inventors

• Lyons Brett I
• Carlson Lisa C
• Stawski Stanley W
• Miller Robert B
• Wallen Matt
• Rossfeldt Jens

Classifications

• B29C70/446

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

• B29C37/0064

  of reinforced material · CPC title

• B29C70/342 Primary

  using isostatic pressure · CPC title

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29L2031/3082

  Fuselages · CPC title