Method and apparatus for forming composite material articles

• US 4,475,976 A
• Filed: 12/23/1983
• Issued: 10/09/1984
• Est. Priority Date: 12/23/1983
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Mittelstadt, Robert F., Stumpf, George R. Jr.
• Primary Examiner(s): Simmons, David A.
• Application Number:
  US06/565,187
• Time in Patent Office: 291 Days
• Field of Search: 156/212, 156/213, 156/382, 156/285-286, 156/221, 156/222, 156/224, 156/226, 264/313, 264/314, 264/316, 264/258, 425/389, 425/390, 100/211
• US Class Current: 156/286
• CPC Class Codes: B29C 43/12 using bags surrounding the moulding material or using membranes contacting the moulding material
• CPC Class Codes: B29C 70/342 using isostatic pressure
• CPC Class Codes: B29C 70/541 Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement positioning inserts in moulds B29C33/12; lay-up on a mould B29C70/30
• CPC Class Codes: Y10T 156/1043 Subsequent to assembly
• CPC Class Codes: Y10T 156/1044 of parallel stacked sheets only

Abstract

A ply (100) of fiber reinforced composite material is laid onto a mandrel (30) having a vacuum ported upper surface with a generally U-shaped cross section. Ply (100) is laid onto the top web (32) of mandrel (30), with its side edges being laid in a cantilevered fashion. A flexible bag (20) is inflated into a stretched condition and lowered over mandrel (30). Bag (20) rolls over mandrel (30) to form play (100) down over mandrel (30). As bag (20) rolls over mandrel (30), it folds ply (100) along two contoured bend lines between the web (32) and flanges (34, 36) of mandrel (30) and simultaneously restrains ply (100) from folding along a straight line. Bag (20) engages a seal (38) carried by mandrel (30). A vacuum is applied through mandrel (30) to evacuate the area between bag (20) and mandrel (30) within seal (38), to compact ply ( 100). Each ply of composite material is formed and compacted before laying another ply.

Claims

1. Apparatus for forming a composite material article having a desired shape, said apparatus comprising:

a mandrel having a vacuum ported upper surface portion that conforms to said desired shape;

a seal carried by the mandrel and surrounding the perimeter of said upper surface portion;

a flexible bag;

inflating means for inflating the bag into a stretched condition;

lowering means for lowering the bag in said condition over said upper surface portion of the mandrel and into sealing engagement with the seal, to form a ply of fiber reinforced composite material that has been laid on said upper surface portion to the shape of said upper surface portion, and for raising the bag out of contact with the mandrel; and

vacuum means for evacuating, through said upper surface portion of the mandrel, the area between the bag and the mandrel and within the seal, to compact said ply.

2. Apparatus as described in claim 1, in which said upper surface portion is contoured.

3. Apparatus as described in claim 1, in which said upper surface portion includes an elongated contoured bend line.

4. Apparatus as described in claim 1, in which said upper surface portion is generally U-shaped in cross section, with a top generally horizontal web and two side generally vertical flanges;

and said seal is generally saddle-shaped.

5. Apparatus as described in claim 4, in which said upper surface portion includes an elongated contoured bend line between said web and each of said flanges.

6. A method of forming a composite material article, comprising:

laying a ply of fiber reinforced composite material onto a vacuum ported mandrel having a shape conforming to the desired shape of the article;

inflating a flexible bag into a stretched condition;

lowering the inflated bag over the mandrel to form the ply to the shape of the mandrel, and bringing a portion of the bag into sealing engagement with a seal carried by the mandrel around the perimeter of the formed ply;

applying a vacuum through the mandrel to the area between the bag and the mandrel and within the seal to compact the ply;

raising the bag to take it out of contact with the mandrel and the ply; and

laying additional plies of fiber reinforced composite material as necessary to obtain a desired thickness, and forming and compacting each such additional ply before laying another ply.

7. A method as described in claim 6, in which the step of lowering the bag to form the ply includes allowing portions of the bag to unstretch to prevent formation of wrinkles, and allowing other portions of the bag to stretch further to prevent bridging.

8. A method as recited in claim 6, in which the step of lowering the bag to form the ply includes allowing the bag to roll over essentially the entire length of an elongated contoured bend line on the mandrel essentially simultaneously, to fold the ply along said bend line and at the same time restrain the ply from folding along a straight line.