Composite core and method of making same

Patent metadata

Field	Value
Publication number	US-9120255-B2
Application number	US-201313835649-A
Country	US
Kind code	B2
Filing date	Mar 15, 2013
Priority date	Mar 15, 2013
Publication date	Sep 1, 2015
Grant date	Sep 1, 2015

Abstract

A method of wrapping a plurality of mandrels with a composite material can include rotating each mandrel at a rotational speed; translating each mandrel at a translation speed; positioning each mandrel back to back such that an aft face of a preceding mandrel is approximate to a forward face of a trailing mandrel; and sequentially wrapping each mandrel with the composite material in a helical orientation.

First claim

The invention claimed is:

1. A method of wrapping a plurality of mandrels with a composite material, the method comprising:
rotating each mandrel at a rotational speed;
translating each mandrel at a translational speed;
positioning each mandrel back to back such that an aft face of a preceding mandrel is approximate to a forward face of a trailing mandrel;
sequentially wrapping each mandrel with the composite material in a helical orientation by selectively positioning a feed head at a wrap angle relative to a translation axis of the plurality of mandrels;
compacting the composite material of each mandrel via a compactor that includes pads that travel in an axial direction of the mandrel and rotate at the same speed as the mandrel, the pads of the compactor pressing against external surfaces of the composite material near aft and forward portions of the mandrel prior to a cutting of the composite material in order to prevent the composite material from unraveling; and
moving the compactor back to align with the next wrapped mandrel.

2. The method according to claim 1 , wherein each mandrel has a hexagonal shape.

3. The method according to claim 1 , further comprising:
banding the composite material near end portions of each mandrel prior to a cutting of the composite material in order to prevent the composite material from unraveling.

4. The method according to claim 1 , further comprising:
stacking each wrapped mandrel.

5. The method according to claim 1 , further comprising cutting the composite material with a laser cutter.

6. The method according to claim 1 , further comprising cutting the composite material with a mechanical cutter.

7. The method according to claim 1 , wherein the step of sequentially wrapping each mandrel with the composite material in the helical orientation includes pulling off the composite material from the feed head by the rotation and translation of each mandrel.

8. The method according to claim 1 , wherein the composite material is a broadgood having a specific width so that each mandrel is wrapped without gaps between adjacent edges of the helically wrapped broadgood.

9. The method according to claim 1 , wherein the composite material is a tow of fibers.

10. The method according to claim 1 , wherein the composite material is a slit tape of composite material.

11. The method according to claim 1 , wherein the composite material is a combination of fibers and uncured resin.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Oldroyd Paul K
• Hethcock Jr James D
• Tohlen Mark E
• Kendrick Phillip A

Classifications

• B29C70/32 Primary

  on a rotating mould, former or core · CPC title

• B29C70/345

  using matched moulds · CPC title

• B29C41/52

  Measuring, controlling or regulating · CPC title

• B29C53/821

  Mandrels especially adapted for winding and joining · CPC title

• B29K2105/0872

  Prepregs · CPC title