Tooling apparatus and method for double-vacuum-bag degassing of a composite layup

Patent metadata

Field	Value
Publication number	US-10118321-B2
Application number	US-201614988528-A
Country	US
Kind code	B2
Filing date	Jan 5, 2016
Priority date	Jan 5, 2016
Publication date	Nov 6, 2018
Grant date	Nov 6, 2018

Abstract

A tooling apparatus for manufacturing a composite structure may include a rigid outer tool for receiving a composite layup, a tubular inner vacuum bag in contact with the composite layup and defining an inner vacuum chamber, and an outer vacuum bag covering at least a portion of the rigid outer tool. The outer vacuum bag and the tubular inner vacuum bag may collectively define an outer vacuum chamber containing the composite layup. An outer bag vacuum source may be fluidly coupled to the outer vacuum bag for applying an outer bag vacuum pressure on the outer vacuum chamber. An inner bag vacuum source may be fluidly coupled to the tubular inner vacuum bag for applying an inner bag vacuum pressure on the inner vacuum chamber during application of the outer bag vacuum pressure on the outer vacuum chamber.

First claim

What is claimed is:

1. A tooling apparatus for manufacturing a composite structure, comprising:
a rigid outer tool configured to receive a tool side of a composite layup;
a tubular inner vacuum bag configured to be placed in contact with a bag side of the composite layup, the tubular inner vacuum bag having an interior defining an inner vacuum chamber;
an outer vacuum bag covering at least a portion of the rigid outer tool such that the outer vacuum bag and the tubular inner vacuum bag collectively define an outer vacuum chamber containing the composite layup;
an outer bag vacuum source fluidly coupled to the outer vacuum bag and configured to apply an outer bag vacuum pressure on the outer vacuum chamber;
an inner bag vacuum source fluidly coupled to the tubular inner vacuum bag and configured to apply an inner bag vacuum pressure on the inner vacuum chamber during application of the outer bag vacuum pressure on the outer vacuum chamber; and
the rigid outer tool separating the outer vacuum bag from at least one of the tubular inner vacuum bag and the composite layup at locations where the tubular inner vacuum bag applies compaction pressure to the bag side of the composite layup.

2. The tooling apparatus of claim 1 , wherein:
the tubular inner vacuum bag extends out of and is sealed to the outer vacuum bag and coupled to the inner bag vacuum source.

3. The tooling apparatus of claim 1 , further including:
a bag carrier positioned inside the tubular inner vacuum bag and supporting the tubular inner vacuum bag during application of an inner bag vacuum pressure on the inner vacuum chamber.

4. The tooling apparatus of claim 1 , wherein:
the rigid outer tool comprises a clamshell mold having a mold lower half and a mold upper half, at least one of the mold lower half and the mold upper half configured to receive the composite layup;
the tubular inner vacuum bag is supported on a bag carrier and positioned between opposing bag sides of the composite layup; and
the mold lower half and the mold upper half configured to be mated together to form the clamshell mold enclosing the composite layup, the bag carrier and the tubular inner vacuum bag.

5. The tooling apparatus of claim 4 , wherein:
the clamshell mold includes a pair of the bag carriers each supporting a tubular inner vacuum bag and defining a respective inner vacuum chamber and positioned on opposite sides of an internal element layup included with the composite layup.

6. The tooling apparatus of claim 1 , wherein:
the composite layup has an airfoil-shaped cross-section including a leading edge and a trailing edge.

7. The tooling apparatus of claim 1 , wherein:
the rigid outer tool comprises a rigid outer plate supported in spaced relation over a layup plate and positioned in non-contacting relation over the composite layup supported on the layup plate; and
the tubular inner vacuum bag positioned between the composite layup and the rigid outer plate.

8. The tooling apparatus of claim 7 , wherein:
the tubular inner vacuum bag includes an inner bag vent tube extending out of the outer vacuum bag and fluidly coupled to the inner bag vacuum source.

9. The tooling apparatus of claim 7 , wherein:
the layup plate has a plate contour for imparting a part contour to the composite layup.

10. A tooling apparatus for manufacturing a composite structure, comprising:
a rigid outer plate supported in spaced relation above a layup plate, the layup plate configured to receive a tool side of a composite layup;
a tubular inner vacuum bag defining an inner vacuum chamber and configured to be positioned between the rigid outer plate and a bag side of the composite layup;
an outer vacuum bag sealing the composite layup and tubular inner vacuum bag to the layup plate, the outer vacuum bag and the tubular inner vacuum bag collectively defining an outer vacuum chamber containing the composite layup and the tubular inner vacuum bag;
an outer bag vacuum source fluidly coupled to the outer vacuum bag and configured to apply an outer bag vacuum pressure on the outer vacuum chamber;
an inner bag vacuum source fluidly coupled to the tubular inner vacuum bag and configured to apply an inner bag vacuum pressure on the inner vacuum chamber during application of the outer bag vacuum pressure on the outer vacuum chamber; and
the rigid outer plate separating the outer vacuum bag from at least one of the tubular inner vacuum bag and the composite layup at locations where the tubular inner vacuum bag applies compaction pressure to the bag side of the composite layup.

11. A tooling apparatus for manufacturing a composite structure, comprising:
a clamshell mold having a mold lower half and a mold upper half configured to respectively receive a lower skin layup and an upper skin layup and an internal element layup extending between a bag side of the lower skin layup and a bag side of the upper skin layup;
a pair of tubular inner vacuum bags each defining an inner vacuum chamber and supported on a bag carrier and positioned between the lower skin layup and the upper skin layup and located on opposite sides of the internal element layup;
an outer vacuum bag covering at least a portion of the clamshell mold such that the outer vacuum bag and the pair of tubular inner vacuum bags collectively define an outer vacuum chamber containing the lower skin layup, the upper skin layup, and the internal element layup;
an outer bag vacuum source fluidly coupled to the outer vacuum bag and controlling an outer bag vacuum pressure within the outer vacuum chamber; and
an inner bag vacuum source fluidly coupled to the tubular inner vacuum bags and controlling an inner bag vacuum pressure within the inner vacuum chamber.

12. A method of manufacturing a composite structure, comprising:
supporting a tool side of a composite layup on a rigid outer tool;
positioning a tubular inner vacuum bag against a bag side of the composite layup, the tubular inner vacuum bag having an interior defining an inner vacuum chamber;
covering, using an outer vacuum bag, at least a portion of the rigid outer tool such that the outer vacuum bag and the tubular inner vacuum bag collectively define an outer vacuum chamber containing the composite layup;
applying an outer bag vacuum pressure to the outer vacuum chamber while applying an inner bag vacuum pressure to the inner vacuum chamber, the inner bag vacuum pressure being no less than the outer bag vacuum pressure; and
drawing gas from the composite layup and out of the outer vacuum bag while applying the outer bag vacuum pressure and the inner bag vacuum pressure, the rigid outer tool separating the outer vacuum bag from at least one of the tubular inner vacuum bag and the composite layup at locations where the tubular inner vacuum bag applies compaction pressure to the bag side of the composite layup.

13. The method of claim 12 , further including:
venting the inner vacuum chamber to atmosphere while continuing to apply the outer bag vacuum pressure to the outer vacuum bag; and
applying compaction pressure of the tubular inner vacuum bag on the bag side of the composite layup as a result of venting the inner vacuum chamber to atmosphere.

14. The method of claim 13 , further including:
maintaining the compaction pressure on the composite layup until the composite layup is cured to form a cured composite structure.

15. The method of claim 12 , wherein the step of applying the inner bag vacuum pressure and the outer bag vacuum pressure includes:
applying the inner bag vacuum pressure at a level substantially equivalent to the outer bag vacuum pressu

Assignees

• Boeing Co

Inventors

• Witte Philipp
• Stawski Stanley W
• Kleshchev Fedor A
• Zarfos Joshua
• Naidu Parth

Classifications

• B64C2001/0072

  from composite materials · CPC title

• B29L2031/3082

  Fuselages · CPC title

• B29C2043/3644

  Vacuum bags; Details thereof, e.g. fixing or clamping · CPC title

• B29C43/3642

  Bags, bleeder sheets or cauls for isostatic pressing · CPC title

• B29C70/44

  using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title