System and method of manufacturing composite core

Patent metadata

Field	Value
Publication number	US-10131108-B2
Application number	US-201313782359-A
Country	US
Kind code	B2
Filing date	Mar 1, 2013
Priority date	Mar 1, 2013
Publication date	Nov 20, 2018
Grant date	Nov 20, 2018

Abstract

A method of manufacturing a composite core can include: wrapping a mandrel in a mandrel wrapping process by securing a mandrel with a winding jig; orienting the composite material at a wrap angle to the mandrel; and depositing the composite material around a circumference of the mandrel. The method can further include assembling the wrapped mandrels in a tool and applying a pressure to the composite material during a curing cycle.

First claim

The invention claimed is:

1. A method of manufacturing a composite core, the method comprising:
wrapping each of a plurality of mandrels with a composite material such that the composite material is wrapped at least 360 degrees around each mandrel;
providing a tool comprising a plurality of partial tools configured to be assembled, each partial tool having an interior surface, an exterior surface, and a plurality of apertures adjacent to the interior surface and disposed between the interior surface and the exterior surface; the plurality of partial tools comprising a first partial tool and a second partial tool;
stacking a first portion of the plurality of mandrels wrapped with the composite material on the interior surface of the first partial tool;
stacking a second portion of the plurality of mandrels wrapped with the composite material on the interior surface of the second partial tool;
assembling the first partial tool and the second partial tool such that some of the plurality of mandrels wrapped with the composite material stacked in the first partial tool are positioned adjacent to some of the plurality of mandrels wrapped with the composite material stacked in the second partial tool; and
curing the composite material in a curing process, the curing process including controllably applying an inward pressure to the assembled first partial tool and second partial tool with an inflatable press bladder;
wherein the plurality of apertures provides a control and tailor thermal expansion of the interior surface on the assembled first partial tool and second partial tool during the curing step.

2. The method according to claim 1 , wherein the exterior surface of each partial tool is an arc of a tool circumference.

3. The method according to claim 1 , wherein the plurality of apertures comprises at least one aperture having a varied circumference from at least one other aperture.

4. The method according to claim 1 , wherein the step of wrapping each of the plurality of mandrels with the composite material includes wrapping a slit of the composite material in a helical path on each of the plurality of mandrels starting from an end portion of each of the plurality of mandrels.

5. The method according to claim 1 , wherein the steps of stacking a first portion and a second portion of the plurality of mandrels wrapped with the composite material includes stacking the first portion of the plurality of mandrels wrapped with the composite material in a pyramid shape on the first partial tool, stacking the second portion of the plurality of mandrels wrapped with the composite material in a pyramid shape on the second partial tool, then subsequently assembling the first partial tool and the second partial tool.

6. The method according to claim 1 , further comprising:
controllably applying a pressure to the tool with a mechanical press during the curing process.

7. The method according to claim 1 , wherein each of the plurality of mandrels is hexagonal shaped.

8. The method according to claim 1 , wherein the step of curing the composite material includes moving a heated fluid through an interior of at least one of the plurality of mandrels to controllably heat the composite material.

9. A method of manufacturing a block of composite core, the method comprising:
wrapping each of a plurality of mandrels with a composite material such that the composite material is wrapped at least 360 degrees around each mandrel;
providing a tool comprising a plurality of partial tools configured to be assembled into a cylindrical shape, each partial tool having an interior surface, an exterior surface, and a plurality of apertures adjacent to the interior surface and disposed between the interior surface and the exterior surface;
stacking a portion of the plurality of mandrels wrapped with the composite material on the interior surface of each partial tool;
assembling the partial tools to create the assembled tool, wherein some of the plurality of mandrels wrapped with the composite material stacked in each partial tool are positioned adjacent to some of the plurality of mandrels wrapped with the composite material stacked in another partial tool; and
controllably applying an inward pressure to the assembled tool with an inflatable press bladder during a curing process;
wherein the plurality of apertures provides a control and tailor thermal expansion of the interior surface on the assembled partial tools during the curing process.

10. The method according to claim 9 , further comprising:
moving a heated fluid through an interior of the plurality of mandrels to controllably heat the composite material in the curing process.

11. The method according to claim 10 , wherein the heated fluid is a gas.

12. The method according to claim 11 , wherein the gas is air.

13. The method according to claim 10 , wherein the heated fluid is an oil.

14. The method according to claim 9 , wherein the exterior surface of each partial tool is an arc of a tool circumference.

15. The method according to claim 9 , wherein the assembled tool comprises six partial tools that are configured to produce a hexagonal shaped core member.

16. The method according to claim 9 , wherein the plurality of apertures comprises at least one aperture having a varied circumference from at least one other aperture.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Kendrick Phillip A
• Oldroyd Paul K
• Armstrong Levi H
• Oberle Elizabeth

Classifications

• B29C2035/046

  dried air · CPC title

• B31C3/00

  Making tubes or pipes by feeding obliquely to the winding mandrel centre line · CPC title

• B29C53/824

  collapsible, e.g. elastic or inflatable; with removable parts, e.g. for regular shaped, straight tubular articles (B29C53/825 takes precedence) · CPC title

• B29D99/0089 Primary

  Producing honeycomb structures (consisting of porous ceramic ware C04B38/0006) · CPC title

• B31D3/0223

  Making honeycomb cores, e.g. by piling a plurality of web sections or sheets · CPC title