Cast components having surfaces with resin coatings

Patent metadata

Field	Value
Publication number	US-11052583-B2
Application number	US-201815871517-A
Country	US
Kind code	B2
Filing date	Jan 15, 2018
Priority date	Jan 15, 2018
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

Abstract

Lightweight and strong components may be manufactured using foam material compositions and resin coating materials by the processes described herein. One or more mandrels and/or a molding tool may be coated with resin coatings, the one or more mandrels may be inserted into the molding tool, and a foam material composition may be injected into the molding tool. After closing the molding tool, the foam material composition may expand and cure to form a component, and heat may be applied to cure the resin coatings into skins. For example, an external skin may be formed by the resin coatings on an exterior surface of the component in contact with surfaces of the molding tool, and one or more internal skins may be formed by the resin coatings on one or more interior surfaces of negative space spars of the component in contact with surfaces of the one or more mandrels.

First claim

What is claimed is:

1. A method of manufacturing a component, comprising:
applying a urethane resin material composition to a mandrel and a molding tool;
inserting the mandrel into the molding tool;
metering a foam material composition into the molding tool;
closing the molding tool for a period of time, wherein the foam material composition expands and cures to form a component having a negative space spar during the period of time;
applying heat to the molding tool during at least a portion of the period of time, wherein the urethane resin material composition cures to form a skin of the component during the at least a portion of the period of time;
opening the molding tool after the period of time;
removing the component from the molding tool; and
removing the mandrel from the negative space spar of the component.

2. The method of claim 1 , wherein the urethane resin material composition applied to the molding tool forms an external skin on an exterior surface of the component during the at least a portion of the period of time.

3. The method of claim 1 , wherein the urethane resin material composition applied to the mandrel forms an internal skin on an interior surface of the negative space spar of the component during the at least a portion of the period of time.

4. The method of claim 1 , wherein the urethane resin material composition comprises at least one of microspheres or pigment.

5. A method, comprising:
applying a resin material composition to a mandrel and a molding tool;
inserting the mandrel into the molding tool;
injecting a foam material composition into the molding tool;
closing the molding tool for a period of time, wherein the foam material composition expands and cures to form a component having a negative space spar during the period of time, and wherein the resin material composition cures to form a skin of the component during at least a portion of the period of time.

6. The method of claim 5 , further comprising:
opening the molding tool after the period of time;
removing the component from the molding tool; and
removing the mandrel from the negative space spar of the component.

7. The method of claim 5 , wherein the resin material composition forms the skin on an interior surface of the negative space spar and an exterior surface of the component during the at least a portion of the period of time.

8. The method of claim 7 , wherein the mandrel includes at least one surface feature that forms a corresponding internal surface feature on the skin of the interior surface of the negative space spar of the component.

9. The method of claim 8 , wherein the at least one surface feature of the mandrel includes at least one corrugation extending along a long axis of the mandrel.

10. The method of claim 8 , wherein the at least one surface feature of the mandrel includes at least one of a rib, protrusion, bump, indentation, or dimple.

11. The method of claim 7 , wherein the resin material composition is applied to the molding tool, and the molding tool includes at least one surface feature that forms a corresponding external surface feature on the skin of the exterior surface of the component.

12. The method of claim 5 , wherein the mandrel is at least one of an inflatable mandrel, adjustable mandrel, or expanding mandrel.

13. The method of claim 5 , further comprising:
inserting a support material into the molding tool prior to at least one of injecting the foam material composition into the molding tool or closing the molding tool for the period of time.

14. The method of claim 13 , wherein the support material includes at least one of a beam, rod, or spar.

15. The method of claim 5 , wherein inserting the mandrel into the molding tool comprises inserting a plurality of mandrels into the molding tool, and wherein the component includes a respective plurality of negative space spars.

16. A method of manufacturing a component, comprising:
applying a first resin material composition to a first surface of a molding tool;
applying a second resin material composition to a second surface of a mandrel;
inserting the mandrel into the molding tool;
metering a foam material composition into the molding tool;
closing the molding tool for a period of time such that:
the foam material composition expands and cures, during the period of time, to form a component having a negative space spar formed by the mandrel;
the first resin material composition in contact with the first surface of the molding tool cures to form an external skin of the component; and
the second resin material composition in contact with the second surface of the mandrel cures to form an interior skin of the component; and

removing the mandrel from the negative space spar of the component.

17. The method of claim 16 , wherein the first surface of the molding tool includes at least one surface feature that forms a corresponding external surface feature on the exterior skin of the component.

18. The method of claim 16 , wherein the second surface of the mandrel includes at least one surface feature that forms a corresponding internal surface feature on the interior skin of the negative space spar of the component.

19. The method of claim 16 , wherein:
applying the second resin material composition to the second surface of the mandrel comprises applying the second resin material composition to a plurality of mandrels; and
inserting the mandrel into the molding tool comprises inserting the plurality of mandrels into the molding tool,
and wherein the component includes a respective plurality of negative space spars.

20. The method of claim 16 , wherein the first resin material composition and the second resin material composition comprise at least one of microspheres, microbeads, or a pigment.

Assignees

• Amazon Tech Inc

Inventors

• Mcginnis Steven
• Glynn Prescott Gee
• Chellabi Kader
• Wallace Adrian Timothy
• Welsh Ricky Dean

Classifications

• B29C33/505 Primary

  cores or mandrels, e.g. inflatable (B29C33/0016 takes precedence; for winding and joining B29C53/824; for supporting articles during joining B29C66/634; flexible cores for vulcanizing tyres B29D30/0654) · CPC title

• B29C33/485

  cores or mandrels (collapsible mandrels for shaping tube ends B29C57/02; collapsible mandrels for winding and joining B29C53/824) · CPC title

• B29C44/355

  Characteristics of the foam, e.g. having particular surface properties or structure · CPC title

• B29C44/14

  the preformed part being a lining {(B29C44/1209 takes precedence)} · CPC title

• B29L2031/3085

  Wings · CPC title