Method of making foam-filled composite products

• US 6,117,376 A
• Filed: 12/09/1997
• Issued: 09/12/2000
• Est. Priority Date: 12/09/1996
• Status: Expired due to Term

• Current Assignee: Michael Merkel
• Original Assignee: Michael Merkel
• Inventors: Merkel, Michael
• Primary Examiner(s): Kuhns, Allan R.
• Application Number:
  US08/987,533
• Time in Patent Office: 1,008 Days
• Field of Search: 264/258, 264/46.5, 264/46.6, 264/46.7, 264/338, 264/257
• US Class Current: 264/46.5
• CPC Class Codes: B29C 44/1233 the preformed parts being supported during expanding
• CPC Class Codes: B29C 44/14 the preformed part being a lining B29C44/1209 takes precedence
• CPC Class Codes: B29C 44/3415 Heating or cooling
• CPC Class Codes: B29C 70/342 using isostatic pressure
• CPC Class Codes: B64C 3/24 Moulded or cast structures
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

A method for making foam-filled parts having fiber-reinforced skins or surfaces is disclosed. Mold halves of pressure-resisting thermally insulative material are covered with a release material, which is then covered with the fiber skins. The fiber skins are coated with heat-curable resin, and the mold halves are then clamped together to form a cavity. A catalyzed foam-forming mixture is poured into the cavity. The mixture foams and expands to the full volume of the cavity, and while it hardens generates heat sufficient to cure the resin.

Claims

1. A method of forming a volumetric part having a pair of fiber-reinforced resin skins about a solid foam interior body, using a pair of mold halves defining the outside configuration of the body, the method comprising the steps of:

laying dry fiber skins in the mold halves to provide skins having substantially coextensive edges along at least two sides;

wetting the skins with heat curable resin;

joining the mold halves together along the coextensive edges to provide an interior volume sealed except for an access aperture;

inserting catalyzed foamable exothermic material into the interior volume through the access aperture after wetting the skins with heat curable resin in an amount that is sufficient to overfill the entire interior volume when foamed;

allowing the exotherm from the foaming to activate and cure the resin for a time sufficient to unite the foamed body to the resin of the skin while exerting expansive force thereon; and

separating the molds from the cured resin skins.

2. A method as set forth in claim 1 above, wherein the mold halves define concavities having substantially parallel side flanges and further including the steps of:

covering the concavities with release material before laying in the dry fiber skins;

plugging one open end of the joined molds before inserting foamable material; and

clamping the molds together along the side flanges to resist pressure buildup.

3. A method as set forth in claim 1 above including the steps of providing sufficient structural reinforcement for the mold halves to resist significant deflection from pressure buildup and sufficient insulation to retain exothermic heat for the desired interval.

4. A method as set forth in claim 2 above, wherein the plugging of one open end comprises inserting a malleable removable material, and the method further includes the steps of placing the access aperture in an elevated position and pouring the foamable material into the interior volume.

5. A method as set forth in claim 1 above, wherein the volumetric part comprises an airfoil, and wherein the method includes raising the exotherm level to above about 300°

F., and further includes the steps of curing the structure for in excess of about one hour, and inserting a release material in the form of sheets against the concavity walls.

6. A method as set forth in claim 1 above, wherein the fiber skins are made of bi-directional plain weave carbon fibers, the resin impregnant is an epoxy resin, the catalyst is thermally activated, and the method further includes the step of precisely positioning the mold halves relative to each other by positioning pins inserted in positioning holes in the side flanges.

7. A method as set forth in claim 1 above, further including placing a removable part within the interior volume of the joined molds prior to inserting the catalyzed exothermic material, and removing said part after curing of the material to form a cavity in the material for insertion of a permanent part.

8. A method as set forth in claim 1 above, further including placing a permanent part within the interior volume of the joined molds prior to inserting the catalyzed exothermic material.